WorldWideScience

Sample records for ballistic missile defense

  1. How to optimize joint theater ballistic missile defense

    OpenAIRE

    Diehl, Douglas D.

    2004-01-01

    Approved for public release, distribution is unlimited Many potential adversaries seek, or already have theater ballistic missiles capable of threatening targets of interest to the United States. The U.S. Missile Defense Agency and armed forces are developing and fielding missile interceptors carried by many different platforms, including ships, aircraft, and ground units. Given some exigent threat, the U.S. must decide where to position defensive platforms and how they should engage poten...

  2. A Two-Sided Optimization for Theater Ballistic Missile Defense

    OpenAIRE

    Brown, G.; Carlyle, M.; Diehl, D; Kline, J.; Wood, K.

    2005-01-01

    Operations Research, 53, pp. 263-275. Center for Infrastructure Defense (CID) Paper. We describe JOINT DEFENDER, a new two-sided optimization model for planning the pre-positioning of defensive missile interceptors to counter an attack threat. In our basic model, a defender pre-positions ballistic missile defense platforms to minimize the worst-case damage an attacker can achieve; we assume that the attacker will be aware of defensive pre-positioning decisions, and that both sides have ...

  3. Theater ballistic missile defense: modeling and analysis of the Marine Corps "HAWK" Missile Defense System

    OpenAIRE

    Monroe, William James Fredrick.

    1995-01-01

    This thesis develops the concept of integrating IDEF modeling with matrix analysis to explore the current state of the Marine Corps, 'As Is', Theater Ballistic Missile Defense information architecture. It demonstrates the possibility of using matrix analysis in conjunction with IDEF modeling to identify deficiencies within an existing information architecture. Using this framework, new technologies and advancements can also be measured to ensure they accurately address deficiencies identified...

  4. Possible allied ballistic missile defense systems: Related guidance and control requirements

    Science.gov (United States)

    Roche, C.; Cotillard, C.

    1995-01-01

    This document discusses several different types of Ballistic Missile Defense Systems for NATO for both medium and long range attacks. The feasibility, technological assessment and forecasting, and defense architecture is presented, along with each system's capabilities.

  5. China and ballistic missile defense: 1955 to 2002 and beyond

    International Nuclear Information System (INIS)

    China's opposition to U.S. ballistic missile defense was forcefully articulated officially and unofficially between 1991 and 2001. Vociferous opposition gave way to near silence following U.S. ABM Treaty withdrawal, raising a question about precisely whether and how China will respond to future U.S. deployments in both the political and military-operational realms. To gauge likely future responses, it is useful to put the experience of the 1991-2001 period into historical context. China's attitudes toward BMD have passed through a series of distinct phases since the beginning of the nuclear era, as China has been concerned alternately with the problems of strategic defense by both the Soviet Union and United States (and others) around its periphery. Throughout this era it has also pursued its own strategic defense capabilities. There are important elements of continuity in China's attitudes concerns about the viability of its own force and about strategic stability. These suggest the likelihood of significant responses to U.S. BMD even in the absence of sharp rhetoric. (author)

  6. China and ballistic missile defense: 1955 to 2002 and beyond

    Energy Technology Data Exchange (ETDEWEB)

    Brad, Roberts

    2004-07-01

    China's opposition to U.S. ballistic missile defense was forcefully articulated officially and unofficially between 1991 and 2001. Vociferous opposition gave way to near silence following U.S. ABM Treaty withdrawal, raising a question about precisely whether and how China will respond to future U.S. deployments in both the political and military-operational realms. To gauge likely future responses, it is useful to put the experience of the 1991-2001 period into historical context. China's attitudes toward BMD have passed through a series of distinct phases since the beginning of the nuclear era, as China has been concerned alternately with the problems of strategic defense by both the Soviet Union and United States (and others) around its periphery. Throughout this era it has also pursued its own strategic defense capabilities. There are important elements of continuity in China's attitudes concerns about the viability of its own force and about strategic stability. These suggest the likelihood of significant responses to U.S. BMD even in the absence of sharp rhetoric. (author)

  7. The science, technology, and politics of ballistic missile defense

    International Nuclear Information System (INIS)

    America's missile defense systems are deployed at home and abroad. This includes the Groundbased Missile Defense (GMD) system in Alaska and California, the Phased Adaptive Approach in Europe (EPAA), and regional systems in the Middle East and Asia. Unfortunately these systems lack workable architectures, and many of the required elements either don't work or are missing. Major review and reconsideration is needed of all elements of these systems. GMD performance in tests has gotten worse with time, when it ought to be getting better. A lack of political support is not to blame as the DoD spends about $10 billion per year, and proposes to add about $5 billion over the next five years. Russia objects to the EPAA as a threat to its ICBM forces, and to the extensive deployment of U.S. military forces in countries such as Poland, the Czech Republic and Romania, once part of the Soviet Union. Going forward the U.S. should keep working with Russia whose cooperation will be key to diplomatic gains in the Middle East and elsewhere. Meanwhile, America's missile defenses face an enduring set of issues, especially target discrimination in the face of attacks designed to overwhelm the defenses, stage separation debris, chaff, decoys, and stealth. Dealing with target discrimination while also replacing, upgrading, or adding to the many elements of U.S. missiles defenses presents daunting budget priorities. A new look at the threat is warranted, and whether the U.S. needs to consider every nation that possesses even short-range missiles a threat to America. The proliferation of missiles of all sizes around the world is a growing problem, but expecting U.S. missile defenses to deal with all those missiles everywhere is unrealistic, and U.S. missile defenses, effective or not, are justifying more and more offensive missiles

  8. Analysis and design of a cooperative weapon assignment module for advanced battle manager of a ballistic missile defense system

    OpenAIRE

    Brown, Willie D.

    2006-01-01

    The United States is in the midst of an ambitious effort to build and deploy a wide range of ballistic missile defense systems. These ballistic missile defense systems will be effective against a host of current and postulated threats from ballistic missiles. In this thesis study, we explore the process of enhancing the effectiveness of weapon assignment for a system of systems. First, analysis of information is drawn from current proposed system of the ABM and its construction from the ...

  9. Design of the Engage Schedule Group for Ballistic Missile Defense%弹道导弹防御的交战程序组设计

    Institute of Scientific and Technical Information of China (English)

    黄树彩; 刘军兰; 康红霞

    2011-01-01

    针对一体化的弹道导弹防御问题,提出了有效进行弹道导弹防御的按程序自动交战原则的交战程序组设计方法.根据一体化的多层弹道导弹防御系统构成,提出了弹道导弹防御交战程序组的概念,设计了实现弹道导弹全程拦截的助推段、中段和末段交战的交战程序组,规划了交战程序组的信息时序.交战程序组的设计对于弹道导弹防御系统的筹划和建设以及系统的作战运用将具有重要的作用.%Aimed at the incorporating ballistic missile defense problem, a design method of Engage Schedule Group is put forward, by using which the auto - engage can be implemented effectivelu according to schedule for ballistic missile defense. Based on the incorporating ballistic missile defense system architecture, the conception of Engage Schedule Group (ESG) for ballistic missile defense is set up. Then the ESGs for ballistic missile boost phase, midcourse phase, and terminal phase intercepting are designed, which are capable of intercepting ballistic missiles in all phases of their flight trajectory. Finally, the information schedules of these ESGs are programmed. The design of ESG is of great value to the plan for and the integration of a ballistic missile defense system and its apphcation.

  10. Soviet debate on missile defense

    Energy Technology Data Exchange (ETDEWEB)

    Parrott, B.

    1987-04-01

    Although the Strategic Defense Initiative (SDI) is meant to cope with the danger of a Soviet nuclear attack, the recent US debate over SDI has paid surprisingly little attention to Soviet views of ballistic missile defense. Despite the existence of a substantial body of pertinent scholarship, the debate has failed to take adequate account of major changes in Soviet ballistic missile defense policy since the mid-1960s. It has also neglected the links between current Soviet military policy and broader Soviet political and economic choices. The Soviets regard SDI not as a novel undertaking to reduce the risks of nuclear war but as an extension of the geopolitical competition between the superpowers. This competition has been dominated in the 1980s, in the Soviet view, by sharply increased US assertiveness and the decline of detente. Viewing SDI as a manifestation of these general trends, Soviet decision makers find the prospect of an unregulated race in ballistic missile defenses and military space technologies deeply unsettling. The deterioration of superpower relations has raised serious doubts in Moscow about the wisdom of Soviet external policy during the 1970s and has provoked sharp internal differences over policy toward the US. Already highly suspicious of the Reagan administration, the elite is united by a general conviction that SDI is an American gambit that may ultimately undercut past Soviet strategic gains and pose a grave new threat to Soviet security. 14 references.

  11. 基于TOPSIS的战区高层反导威胁评估%Threat Assessment of the High Altitude Area Ballistic Missile Defense Based on TOPSIS

    Institute of Scientific and Technical Information of China (English)

    范学渊; 邢清华; 黄沛; 王小光

    2012-01-01

    Firstly, the characteristics of the high altitude area ballistic missile defense' s threat assessment are analyzed. Then the threat assessment's model index system is set up and quantitated, such as launch position of tactical ballistic missile (TBM) , forecasting impact point, range and so on. Finally, the theory of technique for order preference by similarity to idea solution (TOPSIS) based on weight of entropy is used to compute the model. The result shows that the threat assessment' s model and the algorithm is effective and useful for developing the battle manage of the high altitude area ballistic missile defense ' s.%在分析战区高层反导威胁评估特点的基础上,建立了以来袭TBM发射点、预测落点、射程等为核心的战区高层反导威胁评估模型指标体系并进行了相应的量化,然后利用基于熵值权重确定的TOPSIS理论对模型进行求解.通过实例证明所提出的战区高层反导威胁评估模型和算法的有效性,对研究美军的战区高层反导武器系统具有一定的借鉴意义.

  12. Ballistic missile proliferation: An emerging threat 1992

    Energy Technology Data Exchange (ETDEWEB)

    Nagler, R.G.

    1992-10-01

    This report, based solely on information available from unclassified sources, provides a coherent picture of the scope and trends of ballistic missile proliferation. The focus is on countries developing, producing, or owning ballistic missiles capable of threatening the military forces, assets, or populations of neighboring or geographically remote countries. The report also identifies other countries expected to obtain operational ballistic missile capabilities, discusses expected growth in performance, and examines the projected availability of warheads of mass destruction. The emphasis is on ballistic missiles of ranges greater than approximately 300 km, though shorter range battlefield weapons are discussed as forerunners. The assessment excludes principal U.S. allies and countries formerly in the Warsaw Pact, except where these countries have sold missiles, technology; or personnel services to developing nations in support of their missile programs.

  13. Capability Aggregation in the U.S.-Japan Alliance : An assessment of Japan’s impact on U.S. Ballistic Missile Defense (BMD) capabilities

    OpenAIRE

    2011-01-01

    As part of its unprecedented military modernization campaign, China’s development of advanced anti-access capabilities is driving a competition between offensive and defensive missile capabilities in the Asia-Pacific region. Meanwhile, the U.S. is increasingly turning towards its allies, emphasizing the need for strong cooperative relationships and burden sharing in the development of defense architectures against the threat of missile attacks on itself, its deployed troops, and its friends a...

  14. Research on ballistic missile laser SIMU error propagation mechanism

    Institute of Scientific and Technical Information of China (English)

    Wei Shihui; Xiao Longxu

    2008-01-01

    It is necessary that the laser inertial system is used to further improve the fire accuracy and quick reaction capability in the ballistic missile strapdown inertial navigation system. According to the guidance con-trolling method and the output and error model of ballistic missile laser SIMU, the mathematical model of error propagation mechanism is set up and any transfer environmental function of error coefficient that affects the fire accuracy is deduced. Also, the missile longitudinal/lateral impact point is calculated using MATLAB. These estab-lish the technical foundation for further researching the dispersion characteristics of impact point and reducing the laser guidance error.

  15. Civilian casualties of Iraqi ballistic missile attack to Tehran, capital of Iran

    Institute of Scientific and Technical Information of China (English)

    Ali Khaji; Shoaodin Fallahdoost; Mohammad Reza Soroush; Vafa Rahimi-Movaghar

    2012-01-01

    Objective: To determine the pattern of causalities of Iraqi ballistic missile attacks on Tehran,the capital of Iran,during Iraq-Iran war.Methods: Data were extracted from the Army Staff Headquarters based on daily reports of Iranian army units during the war.Results: During 52 days,Tehran was stroked by 118 Al-Hussein missiles (a modified version of Scud missile).Eighty-six missiles landed in populated areas.During Iraqi missile attacks,422 civilians died and 1579 injured (4.9 deaths and 18.3 injuries per missile).During 52 days,8.1 of the civilians died and 30.4 injured daily.Of the cases that died,101 persons (24%) were excluded due to the lack of information.Among the remainders,179 (55.8%) were male and 142 (44.2%) were female.The mean age of the victims was 25.3 years±19.9 years.Our results show that the high accuracy of modified Scud missiles landed in crowded areas is the major cause of high mortality in Tehran.The presence of suitable warning system and shelters could reduce civilian casualties.Conclusion: The awareness and readiness of civilian defense forces,rescue services and all medical facilities for dealing with mass casualties caused by ballistic missile attacks are necessary.

  16. A novel navigation method used in a ballistic missile

    International Nuclear Information System (INIS)

    The traditional strapdown inertial/celestial integrated navigation method used in a ballistic missile cannot accurately estimate the accelerometer bias. It might cause a divergence of navigation errors. To solve this problem, a new navigation method named strapdown inertial/starlight refractive celestial integrated navigation is proposed. To verify the feasibility of the proposed method, a simulated program of a ballistic missile is presented. The simulation results indicated that, when multiple refraction stars are used, the proposed method can accurately estimate the accelerometer bias, and suppress the divergence of navigation errors completely. Specifically, in order to apply this method to a ballistic missile, a novel measurement equation based on stellar refraction was developed. Furthermore a method to calculate the number of refraction stars observed by the stellar sensor was given. Finally, the relationship between the number of refraction stars used and the navigation accuracy is analysed. (paper)

  17. Aerodynamic heating of ballistic missile including the effects of gravity

    Indian Academy of Sciences (India)

    S N Maitra

    2000-10-01

    The aerodynamic heating of a ballistic missile due to only convection is analysed taking into consideration the effects of gravity. The amount of heat transferred to the wetted area and to the nose region has been separately determined, unlike A Miele's treatise without consideration of gravity. The peak heating ratesto the wetted area and to the nose of the missile are also investigated. Finally four numerical examples are cited to estimate the errors, in heat transfers and heating ratesto both wetted area and nose region of the missile, arising out of neglecting the gravitational forces.

  18. The proliferation of ballistic missiles: an aggravating factor of crises

    International Nuclear Information System (INIS)

    After a brief recall of the history of the development of ballistic missiles from World War II, the author discusses the various uses of these missiles, on the one hand by major powers, and on the other hand by other countries like Israel, Pakistan and India, and also Egypt and Iraq. He recalls the uses of these missiles during regional conflicts (Scuds by Iraq) and then discusses the issue of proliferation of ballistic missiles. He notices that most of these weapons are present in the arsenal of major powers under the form of intercontinental missiles, intermediate range weapons or theatre weapons. On the Third World side, proliferation concerns short- and medium-range missiles produced from technology transfers or national programmes. Mobile systems are now present in all conflicts (notably Libya, Syria) and are now based on more advanced technologies for propellers as well as for control and guidance systems. In the last part, the author discusses the perspectives associated with these missiles which are a strong offensive weapon, and are also modernised to carry nuclear warheads or multiple warheads. These evolutions could put the western superiority into question again

  19. Theater missile defense: the effects of TMD on U.S.-Japan security relations

    OpenAIRE

    Spurlock, Kenneth Reace.

    1996-01-01

    This thesis examines the continued pursuit of co-production efforts by the United States with Japan. The President has identified the development of Theater Missile Defenses (TMD) as a priority to counter the proliferation of theater ballistic missiles (TBM) and weapons of mass destruction (WMD). In keeping with the priorities set forth by the President the Secretary of Defense has made several proposals to the Japanese government in regards to the purchase, increased technical exchanges and ...

  20. Robust Hybrid Control for Ballistic Missile Longitudinal Autopilot

    Institute of Scientific and Technical Information of China (English)

    WAEL Mohsen Ahmed; QUAN Quana

    2011-01-01

    This paper investigates the boost phase's longitudinal autopilot of a ballistic missile equipped with thrust vector control.The existing longitudinal autopilot employs time-invariant passive resistor-inductor-capacitor (RLC) network compensator as a control strategy,which does not take into account the time-varying missile dynamics.This may cause the closed-loop system instability in the presence of large disturbance and dynamics uncertainty.Therefore,the existing controller should be redesigned to achieve more stable vehicle response.In this paper,based on gain-scheduling adaptive control strategy,two different types of optimal controllers are proposed.The first controller is gain-scheduled optimal tuning-proportional-integral-derivative (PID) with actuator constraints,which supplies better response but requires a priori knowledge of the system dynamics.Moreover,the controller has oscillatory response in the presence of dynamic uncertainty.Taking this into account,gain-scheduled optimal linear quadratic (LQ) in conjunction with optimal tuning-compensator offers the greatest scope for controller improvement in the presence of dynamic uncertainty and large disturbance.The latter controller is tested through various scenarios for the validated nonlinear dynamic flight model of the real ballistic missile system with autopilot exposed to external disturbances.

  1. A Predictive Explicit Guidance Scheme for Ballistic Missiles

    Directory of Open Access Journals (Sweden)

    N. Prabhakar

    2013-09-01

    Full Text Available A new approach to the design of ballistic missile guidance is presented in this paper. The proposed method uses the missile model to predict the likely impact point at every guidance cycle and apply course corrections based on the predicted impact point (PIP deviations. The algorithm also estimates the in-flight thrust variation from nominal and accordingly updates the model to reduce the uncertainty in the prediction of the impact point. The performance of the algorithm is tested through 6-DOF simulation. The simulation results show excellent performance of the proposed guidance scheme in nominal & off nominal cases.Defence Science Journal, 2013, 63(5, pp.456-461, DOI:http://dx.doi.org/10.14429/dsj.63.2575

  2. Dr. von Braun and Army Ballistics Missile Agency (ABMA) Group

    Science.gov (United States)

    1959-01-01

    This photograph of Dr. von Braun, shown here to the left of General Bruce Medaris, was taken in the fall of 1959, immediately prior to Medaris' retirement from the Army. At the time, von Braun and his associates worked for the Army Ballistics Missile Agency in Huntsville, Alabama. Those in the photograph have been identified as Ernst Stuhlinger, Frederick von Saurma, Fritz Mueller, Hermarn Weidner, E.W. Neubert (partially hidden), W.A. Mrazek, Karl Heimburg, Arthur Rudolph, Otto Hoberg, von Braun, Oswald Lange, Medaris, Helmut Hoelzer, Hans Maus, E.D. Geissler, Hans Heuter, and George Constan.

  3. Ballistic Missile Warhead Recognition based on Micro-Doppler Frequency

    Directory of Open Access Journals (Sweden)

    Sun Hui-Xia

    2008-11-01

    Full Text Available To elucidate the spinning-precession signatures of ballistic warhead, the model of spinning precessionfor ballistic missile warhead is established and the mathematics of micro-Doppler signatures caused by spinning-precession is derived. Then the micro-Doppler features are analysed using high-resolution time-frequencytransform, and the model predictions match the experimental data well. Based on  different mass of warheadsand decoys, the feature, which can reflect the mass of the targets, is extracted from the time-frequency plane,proving a new method for recognising warheads and discriminating these from decoys. Finally the validityof the feature extracted in this study is verified by computer simulations even with low signal-to-noise ratio.Defence Science Journal, 2008, 58(6, pp.705-709, DOI:http://dx.doi.org/10.14429/dsj.58.1697

  4. Cult of deterrence: A moral and strategic critique of the anti-ballistic missile treaty. Master`s thesis

    Energy Technology Data Exchange (ETDEWEB)

    Pringle, C.S.

    1997-12-30

    Ballistic missile defense is the morally and strategically superior alternative to the current system of deterrence, provided that it is responsibly implemented. Analysis of the Just War Criteria and the utilitarian justifications of deterrence present a moral obligation to pursue the alternative strategy of missile defense as a means of defending the United States. However, the Anti-Ballistic Missile (ABM) Treaty does not allow earnest pursuit of this alternative, despite recent efforts to exploit its loopholes and broaden its meaning beyond any reasonable limit. Moreover, deterrence can no longer provide the guarantee of security that it did during the Cold War. Offense-Defense Theory shows that revisionist states are not subject to the same calculations of effective deterrence that the Soviet Union was during that period. This strategic analysis underlies the moral evaluations and further supports missile defense. The cult of deterrence is presented as an explanation for the failure to adapt national security policy to the new international structure, as European powers failed to perceive the offense-defense balance prior to World War I. The ABM regime threatens to reproduce those same mistakes with even greater consequences.

  5. Radar signal analysis of ballistic missile with micro-motion based on time-frequency distribution

    Science.gov (United States)

    Wang, Jianming; Liu, Lihua; Yu, Hua

    2015-12-01

    The micro-motion of ballistic missile targets induces micro-Doppler modulation on the radar return signal, which is a unique feature for the warhead discrimination during flight. In order to extract the micro-Doppler feature of ballistic missile targets, time-frequency analysis is employed to process the micro-Doppler modulated time-varying radar signal. The images of time-frequency distribution (TFD) reveal the micro-Doppler modulation characteristic very well. However, there are many existing time-frequency analysis methods to generate the time-frequency distribution images, including the short-time Fourier transform (STFT), Wigner distribution (WD) and Cohen class distribution, etc. Under the background of ballistic missile defence, the paper aims at working out an effective time-frequency analysis method for ballistic missile warhead discrimination from the decoys.

  6. MEDUSA: A concept for countering multiple targets from theater ballistic missiles. Final report

    Energy Technology Data Exchange (ETDEWEB)

    Peglow, S.G.

    1994-04-01

    We feel that the concept of intercepting a fractionated threat from a tactical ballistic missile is potentially feasible and would have very high payoff for the defense. Many other concepts have been suggested to solve this problem, although they have mostly been more futuristic approaches, e.g. aircrafty based lasers. We also believe that current technologies are not likely to be adequate for the expected types of very small submunition payloads, especially in the presence of relatively simple countermeasures. The MEDUSA concept, or its clones, may very well provide a vehicle for the study of less stressing threats, e.g. separating warheads and provide a lethality enhancement for non-deployed payloads. An opportunity also exists to investigate alternative technologies, such as the explosively-formed ``disk`` idea. The use of high-precision, limited field-of-view sensor-fuzed munitions is a subject of interest in other Defense Department programs and may have application to the important area of theater missile defense.

  7. The proliferation of aerospace weapons technology: Ballistic missiles and the case of Brazil

    Science.gov (United States)

    Vossen, Terrence John

    1993-04-01

    The rationale behind the development of ballistic missile production in Brazil is examined by exploring the political, military, and economic determinants of ballistic missile demand in that country. To ascertain how Brazil developed missile production capabilities, the contributions of aerospace industries in industrialized states, the Brazilian space program, trade between less-developed countries, and illicit trade in missile technology are assessed. It is argued that missile development increasingly became a function of economic as opposed to security considerations, and that technologies transferred from developed country aerospace firms and Brazil's space program were primarily responsible for the creation of production capabilities. It is also contended that the proliferation of missile technology to Brazil was consistent with the workings of a system evident in the aerospace weapons technology market that sustains the horizontal spread of weapons production capabilities.

  8. Application of Extended Kalman Filter to Tactical Ballistic Missile Re-entry Problem

    CERN Document Server

    Bhowmik, Subrata

    2007-01-01

    The objective is to investigate the advantages and performance of Extended Kalman Filter for the estimation of non-linear system where linearization takes place about a trajectory that was continually updated with the state estimates resulting from the measurement. Here tactile ballistic missile Re-entry problem is taken as a nonlinear system model and Extended Kalman Filter technique is used to estimate the positions and velocities at the X and Y direction at different values of ballistic coefficients. The result shows that the method gives better estimation with the increase of ballistic coefficient.

  9. Signature analysis of ballistic missile warhead with micro-nutation in terahertz band

    Science.gov (United States)

    Li, Ming; Jiang, Yue-song

    2013-08-01

    In recent years, the micro-Doppler effect has been proposed as a new technique for signature analysis and extraction of radar targets. The ballistic missile is known as a typical radar target and has been paid many attentions for the complexities of its motions in current researches. The trajectory of a ballistic missile can be generally divided into three stages: boost phase, midcourse phase and terminal phase. The midcourse phase is the most important phase for radar target recognition and interception. In this stage, the warhead forms a typical micro-motion called micro-nutation which consists of three basic micro-motions: spinning, coning and wiggle. This paper addresses the issue of signature analysis of ballistic missile warhead in terahertz band via discussing the micro-Doppler effect. We establish a simplified model (cone-shaped) for the missile warhead followed by the micro-motion models including of spinning, coning and wiggle. Based on the basic formulas of these typical micro-motions, we first derive the theoretical formula of micro-nutation which is the main micro-motion of the missile warhead. Then, we calculate the micro-Doppler frequency in both X band and terahertz band via these micro-Doppler formulas. The simulations are given to show the superiority of our proposed method for the recognition and detection of radar micro targets in terahertz band.

  10. Cooperative Monitoring Center Occasional Paper/9: De-Alerting Strategic Ballistic Missiles

    Energy Technology Data Exchange (ETDEWEB)

    Connell, Leonard W.; Edenburn, Michael W.; Fraley, Stanley K.; Trost, Lawrence C.

    1999-03-01

    This paper presents a framework for evaluating the technical merits of strategic ballistic missile de-alerting measures, and it uses the framework to evaluate a variety of possible measures for silo-based, land-mobile, and submarine-based missiles. De-alerting measures are defined for the purpose of this paper as reversible actions taken to increase the time or effort required to launch a strategic ballistic missile. The paper does not assess the desirability of pursuing a de-alerting program. Such an assessment is highly context dependent. The paper postulates that if de-alerting is desirable and is used as an arms control mechanism, de-alerting measures should satisfy specific cirteria relating to force security, practicality, effectiveness, significant delay, and verifiability. Silo-launched missiles lend themselves most readily to de-alerting verification, because communications necessary for monitoring do not increase the vulnerabilty of the weapons by a significant amount. Land-mobile missile de-alerting measures would be more challenging to verify, because monitoring measures that disclose the launcher's location would potentially increase their vulnerability. Submarine-launched missile de-alerting measures would be extremely challlenging if not impossible to monitor without increasing the submarine's vulnerability.

  11. Robust Graded Sliding Mode Tracking Control for Low Speed Spinning Ballistic Missiles

    Institute of Scientific and Technical Information of China (English)

    ZHOU Jun; WANG Zhi; ZHOU Feng-qi

    2007-01-01

    The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-scale separation of missile dynamics, a graded sliding mode controller is designed with two sub-sliding surfaces which have invariability to external disturbances and parameter perturbations, and a matrix which comprises three first order low pass filters is introduced to prevent "explosion of terms". Owing to the upper bounds of the uncertainties are difficult to obtain in advance,adaptive laws are introduced to estimate the values of the uncertainties in real-time. Eventually, the numerical simulation results given to show the proposed controller can ensure the steady flight of missiles.

  12. 基于RCS的弹道导弹中段目标联合识别研究%Simulation of RCS of ballistic missile warhead

    Institute of Scientific and Technical Information of China (English)

    戴军; 方晖; 张兴敢

    2015-01-01

    弹道导弹中段目标识别是导弹防御系统的核心环节。中段目标外形简单,特征不明显,干扰较多,但是在实际防御过程中,导弹飞行中段是反导防御最适合阶段,因此需要研究新的导弹中段目标特征。本文研究基于动态雷达散射截面积(RCS)的中段目标联合识别方法。在实际仿真过程中,本文以美国民兵洲际导弹作为模型,进行实物尺寸的 RCS仿真。根据弹道导弹在中段飞行中特有的进动特点,给出设定场景条件,得到目标在该场景下的 RCS动态特性。最后根据得到的仿真数据,对弹道导弹中段动态目标识别提出了一种新的可行性方法。%The midcourse of ballistic missile target recognition is a key segment of the Missile Defense System. The target shape is simple and its characteristic is not obvious,with more interference. But from a practical defense process,missile midcourse flight is the most suitable anti missile defense stage. Therefore its needs to study the new characteristics of the missile warhead. Based on the dynamic radar cross section(RCS),this paper researches a joint identification midcourse target method. In the actual simulation process,with the American Minuteman intercontinental missile as a model,the RCS simulation uses the physical size of the missile. According to the characteristics of ballistic missiles in the middle of precession characteristic in flight,the setting scene conditions are given. And the dynamic characteristics of RCS of the target in the scene are obtained. According to the data obtained,the mid-course target combined identification is put forward. A new feasible method for ballistic missile dynamic object recognition is proposed.

  13. Integrating Technologies to Protect the Home Front against Ballistic Threats and Cruise Missiles

    Directory of Open Access Journals (Sweden)

    Yossi Arazi

    2013-12-01

    Full Text Available This article discusses active protection in response to the rocket threat to Israel’s home front. The defense establishment anticipates that in an allout war, the home front would be attacked for about thirty days, and that every day there would be about one thousand rocket and missile hits that would cause thousands of casualties as well as damage to infrastructures and strategic sites. Israel has an active protection system with five layers of interceptor missiles, and in cooperation with the United States, it developed Nautilus, a chemical-laser-based defense system from which the Skyguard system is derived. In 2007, the Iron Dome system, whose missiles are more expensive, was chosen over it for reasons both economic and operational. Yet only an integrated response that includes anti-missile defense systems and chemical laser systems will offer a comprehensive solution for active protection against all threats, without causing any significant economic difficulties.

  14. Minimum Ballistic Factor Missile Shapes For Variable Skin Friction Coefficient

    Directory of Open Access Journals (Sweden)

    S. C. Jain

    1973-10-01

    Full Text Available Minimum ballistic factor for slender axisymmetric power law bodies have been obtained by taking a variable skinfriction coefficient for the cases when any two of the three quantities length, diameter and surface area have been pre-prescribed.

  15. Application of fleet ballistic missile components/designs for expendable launch vehicles

    Science.gov (United States)

    Grizzell, Norman E.

    This paper describes the orbital performance and configuration attributes of an expendable launch vehicle (ELV) derived from flight-qualified components. Representative logistical and programmatic data are also provided. The backbone of the ELV program described is the cost-effective use of proven Fleet Ballistic Missile components/designs coupled with other high confidence 'off-the-shelf' equipment. The ELV defined can place over a thousand pounds (1000 lb) of spacecraft (payload) into Low Earth Orbit.

  16. Tactical unmanned aerial vehicles in a proposed joint infrastructure to counter theater ballistic missiles

    OpenAIRE

    Junker, Vernon L.

    1995-01-01

    Proliferation of tactical ballistic missile (IBM) systems throughout the Third World represents a serious threat to American national interests. As demonstrated during operation Desert Storm in Iraq, countering this threat is a very difficult problem. A joint, multi-level infrastructure to counter the TBM threat is vital to American security. This thesis considers the joint infrastructure and tactics necessary to counter the TBM threat. During peacetime, infrastructure assets monitor TBM forc...

  17. 15 CFR 744.3 - Restrictions on Certain Rocket Systems (including ballistic missile systems and space launch...

    Science.gov (United States)

    2010-01-01

    ... 15 Commerce and Foreign Trade 2 2010-01-01 2010-01-01 false Restrictions on Certain Rocket Systems (including ballistic missile systems and space launch vehicles and sounding rockets) and Unmanned Air...: END-USER AND END-USE BASED § 744.3 Restrictions on Certain Rocket Systems (including ballistic...

  18. The art and science of missile defense sensor design

    Science.gov (United States)

    McComas, Brian K.

    2014-06-01

    A Missile Defense Sensor is a complex optical system, which sits idle for long periods of time, must work with little or no on-­board calibration, be used to find and discriminate targets, and guide the kinetic warhead to the target within minutes of launch. A short overview of the Missile Defense problem will be discussed here, as well as, the top-level performance drivers, like Noise Equivalent Irradiance (NEI), Acquisition Range, and Dynamic Range. These top-level parameters influence the choice of optical system, mechanical system, focal plane array (FPA), Read Out Integrated Circuit (ROIC), and cryogenic system. This paper will not only discuss the physics behind the performance of the sensor, but it will also discuss the "art" of optimizing the performance of the sensor given the top level performance parameters. Balancing the sensor sub-­systems is key to the sensor's performance in these highly stressful missions. Top-­level performance requirements impact the choice of lower level hardware and requirements. The flow down of requirements to the lower level hardware will be discussed. This flow down directly impacts the FPA, where careful selection of the detector is required. The flow down also influences the ROIC and cooling requirements. The key physics behind the detector and cryogenic system interactions will be discussed, along with the balancing of subsystem performance. Finally, the overall system balance and optimization will be discussed in the context of missile defense sensors and expected performance of the overall kinetic warhead.

  19. Brief Study on Penetration Capability of SSBN Launched Ballistic Missile Based on Probability Model%基于概率模型的潜射弹道导弹突防能力初探

    Institute of Scientific and Technical Information of China (English)

    孙东平; 荣海洋; 野学范; 周宝林

    2012-01-01

    In order to quantify penetration capability of SSBN launched ballistic missiles, and directly display the evaluating results, the mathematics analytical method was adopted. Based on the fact of ballistic missile defense system, the penetration capability of SSBN launched ballistic missiles should be calculated at the middle phase and terminal phase. The evaluating results show that the mathematics analytical method could ensure the quantitative assessment on the penetration capability of the SSBN launched ballistic missiles objectively. The conclusions could provide reference for development and improvement of SSBN launched ballistic missiles, and provide basis for submarine army on the utilization of the SSBN launched ballistic missiles.%为了更好地对潜射弹道导弹的突防能力进行定量评估,直观显示评估结果,采用数学解析的方法对其突防能力进行定量评估.根据弹道导弹防御系统的实际情况,只考虑潜射弹道导弹在中段和末段进行突防时的突防能力.从评估结果可以看出,数学解析方法能够较为客观地对潜射弹道导弹的突防能力进行定量评估,为潜射弹道导弹的发展和改进提供参考,并为潜艇部队使用潜射弹道导弹提供依据.

  20. A Study on Ballistic Missile Early Warning Information Processing System%弹道导弹预警信息处理系统研究

    Institute of Scientific and Technical Information of China (English)

    李旭东

    2011-01-01

    随着新军事技术的飞速发展,弹道导弹已经成为世界各军事强国进行现代局部战争首先或重点使用的进攻性武器.单个传感器只能提供导弹飞行某一阶段的信息,不能满足上升段、中段或末段指挥和拦截的要求.文中从弹道导弹防御的全程预警出发,探讨了预警信息处理系统在整个防御过程中的功能和信息流程和需要解决的关键技术,并指出了预警信息处理系统在弹道导弹防御中的重要作用.%Along with new military technology developing rapidly, ballistic missile has become the first and important attack weapon used. A single sensor can only provide a certain information of missile flight, which can not satisfy the requirement of command & control and interception at ascent phase, midcourse phase and terminal phase. Based on early waming of all phases for ballistic missile defense, the functions and information flow and key technologies of early waming information pmcessing system in all defense phases are discussed, and it is shown that the information processing system play an impartant role in hallistic missile defense.

  1. REALIZATION OF GPS/SST/SINS INTEGRATED NAVIGATION FILTER ALGORITHM FOR BALLISTIC MISSILE

    Institute of Scientific and Technical Information of China (English)

    KANGGuo-hua; LIUJian-ye; ZHUYan-hua; XIONGZhi

    2005-01-01

    Considering the domestic single navigation system of the ballistic missile, a new filter method is presented. The method integrates the information of the strapdown star tracker (SST) attitude, the position and the velocity of a high speed GPS with a strapdown inertial navigation system (SINS) information into one filter, thus improving the precision of the attitude, the velocity, and the position. Finally, the GPS/SST/SINS simulation platfornt is designed. Simulation results demonstrate that the filter is robust and reliable, and the precision rises to the comparative level abroad.

  2. Study on the Spline Filter Algorithm in Ballistic Missile Boost-phase%弹道导弹主动段样条滤波算法

    Institute of Scientific and Technical Information of China (English)

    张峰; 田康生

    2012-01-01

    对弹道导弹主动段进行跟踪是弹道导弹主动段防御中极其重要的任务,它是制导拦截的基础.针对传统方法在弹道导弹主动段跟踪能力不足,建立了弹道导弹主动段样条滤波算法.该滤波算法首先用样条函数建立了主动段运动模型,其次在此基础上将运动状态进行了解耦,建立了状态方程,最后基于解耦模型,应用Kalman滤波进行了状态估计,并且在估计中设计了模型更新方法,使算法具有很好的机动跟踪性能.仿真实验证明,该跟踪算法估计精度高于其它算法.%The tracking of ballistic missile under boost-phase is extremely important in the missile early defense program. It is the base of interception. In respect that traditional methods have essential deficiency on the tracking of ballistic missile under boost-phase, this paper introduces a filter algorithm based on spline modeling. First, a ballistic missile under boost-phase motion model is established based on spline function. Then movement state is decoupled. Equation of State is established. At last, based on the decoupling model, state is estimated by using Kalman Filter. This paper has designed a model updating method in order to make it capable of maneuver target tracking. The simulation result shows that this algorithm has high precision and good performance.

  3. Ballistic Model and Simulation of a Light Anti-tank Missile Replication Hitting on Top of Tank at Terminal Trajectory

    Institute of Scientific and Technical Information of China (English)

    SONG Zhen-duo; XU Wen-xu; DIAO Qing

    2006-01-01

    Puts forward a design project of light anti-tank missile controlled by gesture replication at the terminal trajectory, and it can hit the top of tank. The paper studies the closed-loop control rigid ballistic model and simulation for the straight and fleeting flight and terminal replication trajectory for both fixed and moving targets. Simulation results show the program to be practicable.

  4. Determination of the Trajectory of Ballistic Missiles Using a Dense GPS Array

    Science.gov (United States)

    Heki, K.; Ozeki, M.

    2009-12-01

    The dense array of ~1000 Global Positioning System (GPS) receivers in Japan provides useful information on atmosphere and ionosphere in terms of delays of microwaves in propagation media. Here we introduce its brand-new application, determination of the trajectories of ballistic missiles by using their electron depletion signatures in ionosphere. Booker (1961) first detected F-region ion depletion associated with a missile passage. Later, formation of an ionospheric hole by the launch of Skylab was observed, and Mendillo et al. (1975) attributed the electron depletion to the water molecules in the rocket exhaust. In Japan, ionospheric depletion after the launch of the H-IIA rocket was observed at GPS receivers in southern Japan using differences in phases between the two carrier frequencies L1 and L2 (Furuya & Heki, 2008). The so-called Taepodong-1, and -2 (the North Korean government claims that they successfully launched satellites), ballistic missiles with liquid fuel engines, were launched from Musudanri, North Korea, in August 1998, and April 2009, respectively. Their first stage engines splashed down onto the Japan Sea, and their second stage engines flew over northeastern Japan and reached the Pacific Ocean. We investigated GPS data before and after the launches, and detected that linear electron depletion areas appear in the northern part of the Japan Sea (~300 km east of the launch pad) approximately six minutes after the launch. Such electron depletion occurs as a result of exchange of positive charges between oxygen ions and water molecules, and dissociative recombination of water with electrons. The ionospheric hole rapidly grows and gradually decays as the water molecules diffuse. By comparing the numerical simulation results of ionospheric hole formation (water diffusion and chemical reaction) and the observed change in ionospheric total electron content (TEC), we conclude that the Taepodong-1 exhaust included water molecules ~0.5 percent of those in

  5. Design of a Coordinate-Transformation Extended Robust Kalman Filter for Incoming Ballistic Missile Tracking Systems

    Energy Technology Data Exchange (ETDEWEB)

    Shin, J.G. [LG Electronics, Seoul (Korea); Lee, T.H.; Park, J.B. [Yonsei University, Seoul (Korea); Yoon, T.S. [Changwon University, Changwon (Korea); Choi, Y.H. [Kyonggi University, Suwon (Korea)

    2003-01-01

    A Coordinate-Transformation Extended Robust Kalman Filter (CERKF) designed in the Krein space is proposed, and then applied to a nonlinear incoming ballistic missile tracking system with parameter uncertainties. First, the Extended Robust Kalman filter (ERKF) is proposed to handle the nonlinearity of measurement equation which occurs whenever the polar coordinate system is transformed into the Cartesian coordinate system. Moreover, linearization error inevitably occurs and deteriorates the tracking performance, which is considerably reduced by the proposed CERKF. Through the simulation results, we show that the proposed CERKF, which uses the measurement coordinate system, has less RMS error than the previous ERKF which is designed in the Krein space using the Cartesian system. We also verify that the robustness and the stability of the proposed filter are guaranteed in two radars: the phased array radar and the scanning radar. (author). 9 refs., 5 figs.

  6. Elimination of ballistic missiles: An important step towards a nuclear-weapon-free world

    International Nuclear Information System (INIS)

    Although the Non-Proliferation Treaty preamble emphasises 'the elimination from national arsenals of nuclear weapons and the means of their delivery pursuant to a Treaty on general and complete disarmament under strict and effective international control', the Non-Proliferation Treaty does not further specify how this ultimate goal could be achieved for delivery systems. Delivery systems are an important and costly part of nuclear weapons which should be sophisticated, therefore the control of nuclear-capable delivery systems would be an important step to make nuclear weapons useless and reduce the threat od their use. This is especially true for ballistic missiles, which represent effective and powerful means to deploy nuclear weapons

  7. 76 FR 4322 - Availability of the Fiscal Year 2009 Missile Defense Agency Services Contracts Inventory Pursuant...

    Science.gov (United States)

    2011-01-25

    ... of the Secretary Availability of the Fiscal Year 2009 Missile Defense Agency Services Contracts... United States Code as amended by the National Defense Authorization Act for Fiscal Year 2008 (NDAA 08... Procurement and Acquisition Policy, Office of Strategic Sourcing (DPAP/SS) will make available to the...

  8. Target Identification Technique Using in the Ballistic Missile%目标识别技术在弹道导弹防御中的应用

    Institute of Scientific and Technical Information of China (English)

    康成刚; 伍光新; 王建明; 雷新宇; 周伟光; 王其冲

    2012-01-01

    根据弹道导弹目标在飞行中段和再入段的特征差异,给出了目标散射特性、结构特性、姿态特性等的综合识别策略,讨论了基于回波幅度序列、微动特征、质阻比、极化等特征量和雷达成像的目标识别技术在弹道导弹防御中的应用,并初步分析了各种措施的可行性.研究表明,综合应用各种识别手段可以大大提高对抗环境下真假弹道导弹目标的识别能力.%In this paper, synthesis target identification strategy based on scattering character, and structure character gesture character was presented, according to character difference of the ballistic missile target in coast phase and reentry phase. Target identification techniques based on radar cross section, micro-motion character, mass-to-drag ratio, polarization character, and radar imaging applying in the ballistic missile defense were investigated, and their feasibility were analyzed. Simulation for radar target identification method using different characters indicated that with the research on radar target character developed deep and deep, target identification technique synthetically applying the different identification measures can greatly improve the ability of identifying true and false warhead in the electronic war condition.

  9. Study on Method for Simultaneously Tracking and Classifying Ballistic Missile in Boost and Post-boost Phase%弹道导弹助推段同时跟踪和类型识别算法研究

    Institute of Scientific and Technical Information of China (English)

    陈映; 程臻; 文树梁

    2011-01-01

    It is meaningful to tracking ballistic missile in boost phase precisely by forward ground-based radar for the whole antimissile defensive system. The paper presents a new method to track ballistic missile in boost and post-boost phase based on prior database. At first, the paper extracts characteristic dynamic parameters of ballistic missile, and analyzes the sensitivities of these parameters and gives a time invariant dynamic model with parameters; then the paper simulates the performance for tracking ballistic missile in boost and post-boost phase with IMM and IUF algorithm. Compared with other dynamic models and algorithms, this new method has much higher tracking precision and by calculating the model transition prohabilities, it can classify the ballistic missiles and indicates the burnout time accurately. The simulation results validate the new method.%前置地基雷达跟踪助推段弹道导弹对整个反导防御系统有着重要意义.本文提出了一种以情报数据库为先验知识的弹道导弹助推段及后助推段跟踪方法.首先从动力学角度提取导弹助推段飞行的特征参量,并对参量的敏感度进行了分析,给出了一种参变的助推段弹道导弹时不变运动模型.然后结合交互式多模型(IMM)和迭代无敏滤波(IUF)算法进行助推段及后助推段弹道导弹跟踪仿真.与采用其他的运动模型和滤波算法相比,该方法能实现对弹道导弹助推段及后助推段更高精度的跟踪,同时结合情报数据库通过计算模型转移概率可完成导弹类型初判别,并准确指示导弹关机时刻.文章通过仿真验证了该算法的有效性.

  10. 遭毁伤导弹弹道特性仿真分析%Simulation Analysis of Ballistic Characteristic of Damaged Missile

    Institute of Scientific and Technical Information of China (English)

    李向荣; 童睆; 贺金丽

    2009-01-01

    Aiming at the problem of construct damage resulting in the yaw of missile, six-free-degree ballistic simulation of damaged missile is carried out. Six-free-degree movement equations for the missile are established, and ballistic simulation system for the missile is developed by real-time simulation platform of Matlab/Simulink. Based on the simulation results, terminal state and flight track of damaged missile are analyzed. This is significant to new anti-missile technology development.%针对结构毁伤引起导弹偏航问题, 进行了遭毁伤导弹六自由度全弹道数字仿真分析.建立了导弹六自由度运动方程组, 在Matlab/Simulink实时仿真平台下开发了导弹全弹道数字仿真系统, 进行了遭毁伤导弹终点状态和飞行轨迹特性分析, 研究结果对新型反导技术发展具有一定参考价值.

  11. Modular Open System Architecture for Reducing Contamination Risk in the Space and Missile Defense Supply Chain

    Science.gov (United States)

    Seasly, Elaine

    2015-01-01

    To combat contamination of physical assets and provide reliable data to decision makers in the space and missile defense community, a modular open system architecture for creation of contamination models and standards is proposed. Predictive tools for quantifying the effects of contamination can be calibrated from NASA data of long-term orbiting assets. This data can then be extrapolated to missile defense predictive models. By utilizing a modular open system architecture, sensitive data can be de-coupled and protected while benefitting from open source data of calibrated models. This system architecture will include modules that will allow the designer to trade the effects of baseline performance against the lifecycle degradation due to contamination while modeling the lifecycle costs of alternative designs. In this way, each member of the supply chain becomes an informed and active participant in managing contamination risk early in the system lifecycle.

  12. The Peak of Rocket Production: The Designer of Ballistic Missiles V.F. Utkin (1923-2000)

    Science.gov (United States)

    Prisniakov, V.; Sitnikova, N.

    2002-01-01

    achievements V. Utkin and his pupils are crea- tion unique "mortar" launching of a heavy liquid rocket from shaft, the decision of a complex of prob- lems on maintenance ready for military action (continuous attendance) of liquid rockets in the filled condi-tion for many years, maintenance of stability of rockets at action on them of striking factors of nuclear explosion. With personal participation of academician IAA V. Utkin the following large scien- tific and technical results were received: (a) a military railway rocket complex with intercontinental solid-propellant rocket with starting weight of 105 tons and with 10 warheads; (b) a method of war manage-ment with the help of command rockets; (c) a method of definition of characteristics of means of overcoming of antimissile defense; (d) war intercontinental rockets with the increased accuracy, with the survivability, with the availability for action; (e) a commanding rocket. Design' decisions not ha- ving the analogues in world: (a) managements of flight solid-propellant an intercontinental ballistic missiles by means of a deviating head part; (b) managements solid-propellant rocket by method of inje- ction of gas in supercritical part of nozzle; (c) industrial introduction of the newest materials etc.V. Ut- kin is the active participant of works in the field of the international cooperation in research and deve- lopment of a space. In 1990 V. Utkin hold a high post of the director of ZSNIIMACH which is leading organization of a space-rocket industry of Russia. Under manual V. Utkin the Federal space program of Russia was developed. V. Utkin had huge authority as the chairman of Advice of the Main designers of the USSR. He was the co-chairman combined commission of experts V. Utkin - T. Stafford" on problems of maintenance joint manned flights. He was the chairman of Coordination advice under the program of researches on manned space complexes. V. Utkin dreamed to be the active participant of a new stage of the outer

  13. The Regional Dimension of Romania's Participation to the Anti-Missile Defense System

    Directory of Open Access Journals (Sweden)

    Florin Iftode

    2015-08-01

    Full Text Available The current security environment is characterized by a high degree of instability and unpredictability, through the manifestation of new risks and threats, especially those with asymmetrical nature, by redefining the relations between the great powers, and increasing freedom of action of the regional actors (state and non-state. At the international level, the end of the Cold War has led to a fragmentation of efforts in the security field, with direct implications on the need for further efforts of the international community coordination. In this era of profound change and transformation it is not possible the adoption of an isolationist policy of security, but only in a broader context of interdependencies and relationships between general trends, threats or challenges specific to a particular area or geographic areas. Swift operationalization of the anti-missile system will strengthen the national security both directly, through the protection it provides for the entire national territory, and indirectly, as the system will have a deterrent important role, able to mitigate risks of possible attacks by ballistic missiles. The role of deterrence will remove the risk of attack against any Allied territory on which, by virtue of membership in NATO and obligations involved according to article 5 of the Washington Treaty, Romania has also responsibilities.

  14. 弹道导弹威胁估计模型构建%Research on Model Building of Ballistic Missile Threat Assessment

    Institute of Scientific and Technical Information of China (English)

    朱艺; 肖兵; 林傲; 张锋; 王海燕

    2016-01-01

    简要分析了弹道导弹飞行3个阶段的不同特点及各阶段导弹预警探测手段的侧重点,结合威胁估计的特征构建了弹道导弹威胁估计模型结构框架,运用多阶段贝叶斯网络理论,构造了主动段、自由段和再入段威胁估计模型,并明确了三阶段间的转换时机。采用动态贝叶斯方法对弹道导弹作战全过程进行威胁估计仿真推理,仿真结果能够反映导弹在飞行过程中威胁程度的变化特点,为反导指挥员作出辅助决策提供智力支持。%This paper briefly introduces different features in three phases of ballistic missile and focuses in different detection methods of missile early warning according to the features of threat assessment ,It establishes the threat assessment model pattern of ballistic missile. Through applying multi-phase Bayesian theory ,it builds a assessment model which includes boost phase,free phase,and re-entry phase and clarifies proper transformation opportunity among three phases. Besides ,it reasons and simulates the whole battle process of ballistic missile so as to get threat assessment results which reveals the traits of missiles regarding to changes during the flight and to offer intelligent assistance working as auxiliary decisions to commanders.

  15. Method for Tracking Ballistic Missile on Boost Phase%一种适用于助推段弹道导弹的跟踪方法研究

    Institute of Scientific and Technical Information of China (English)

    陈映; 文树梁; 程臻

    2012-01-01

    弹道导弹在助推段的运动特性较为复杂,且由于各级助推器的脱落导弹的加速度存在突变点,在导弹关机时刻的加速度突变最大,因此在跟踪时容易产生较大滤波偏差。本文主要对弹道导弹助推段的加速度特性进行了分析,选择CJ模型来描述其运动特性,采用交互式多模型(IMM)和无敏滤波(UF)算法对处于助推段的弹道目标进行跟踪。由仿真结果可以看出本文所提出的基于CJ模型和CA模型组合的IMM-UF跟踪方法可以较好地实现对助推段弹道导弹的跟踪。同时通过模型集合中各模型的概率变化情况可以很好地完成对导弹关机时刻的判定,这为后续尽早定轨和轨道预报等提供了前提。该算法结构简单实现稳定,具有较好的工程应用价值。%The dynamic feature of ballistic missile in boost phase is sophisticated,and its acceleration changes abruptly when each booster burns out,which results in big filtering bias.The acceleration characteristic of ballistic missile in boost phase was analyzed,and CJ model as the dynamic model of ballistic missile was chosen,IMMUF to track ballistic missile in boost phase was adopted.The simulation result indicates the IMM-UF algorithm based on combination of CJ models and CA model is applicable to track ballistic missile in boost phase.At the same time,the burnout time of BM can be estimated through the probabilities changing of models in model-bank,which provides the foundation for early orbit determination and prediction.This algorithm has good engineering value with simple structure and stable realization.

  16. 导弹末端弹道拟合方法研究%Missile Terminal Ballistic Curve Fitting Methods

    Institute of Scientific and Technical Information of China (English)

    袁震宇; 钟志通; 张林; 张宇

    2015-01-01

    导弹末端弹道估计问题可转换为空间直线拟合问题,通过比较解决空间直线拟合问题的一般最小二乘算法、整体最小二乘算法和主成分分析法,得出使用主成分分析法进行空间直线拟合,理论严密,使用幂法对主成分分析法进行求解,计算简单。算例分析结果表明了主成分分析法求解空间直线拟合问题的可行性和有效性。%The missile terminal ballistic curve estimation can be transferred to be a linear fitting problem .Based on the comparison of general least square algorithm ,total least square algorithm and principle component analysis ,it is concluded that linear fitting using principle analysis is rigid reasoning ,and solving the principle analysis by power method computation cost less .At the end ,an example solving result indicates the feasibility and validity of the principle analysis method which is used to solve the 3‐dimention linear fitting .

  17. Calibration of IR test chambers with the missile defense transfer radiometer

    Science.gov (United States)

    Kaplan, Simon G.; Woods, Solomon I.; Carter, Adriaan C.; Jung, Timothy M.

    2013-05-01

    The Missile Defense Transfer Radiometer (MDXR) is designed to calibrate infrared collimated and flood sources over the fW/cm2 to W/cm2 power range from 3 μm to 28μ m in wavelength. The MDXR operates in three different modes: as a filter radiometer, a Fourier-transform spectrometer (FTS)-based spectroradiometer, and as an absolute cryogenic radiometer (ACR). Since 2010, the MDXR has made measurements of the collimated infrared irradiance at the output port of seven different infrared test chambers at several facilities. We present a selection of results from these calibration efforts compared to signal predictions from the respective chamber models for the three different MDXR calibration modes. We also compare the results to previous measurements made of the same chambers with a legacy transfer radiometer, the NIST BXR. In general, the results are found to agree within their combined uncertainties, with the MDXR having 30 % lower uncertainty and greater spectral coverage.

  18. A new method of passive counting of nuclear missile warheads -a white paper for the Defense Threat Reduction Agency

    Energy Technology Data Exchange (ETDEWEB)

    Morris, Christopher [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Durham, J. Matthew [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Guardincerri, Elena [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Bacon, Jeffrey Darnell [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Wang, Zhehui [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Fellows, Shelby [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Poulson, Daniel Cris [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Plaud-Ramos, Kenie Omar [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Daughton, Tess Marie [Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Johnson, Olivia Ruth [Los Alamos National Lab. (LANL), Los Alamos, NM (United States)

    2015-07-31

    Cosmic ray muon imaging has been studied for the past several years as a possible technique for nuclear warhead inspection and verification as part of the New Strategic Arms Reduction Treaty between the United States and the Russian Federation. The Los Alamos team has studied two different muon imaging methods for this application, using detectors on two sides and one side of the object of interest. In this report we present results obtained on single sided imaging of configurations aimed at demonstrating the potential of this technique for counting nuclear warheads in place with detectors above the closed hatch of a ballistic missile submarine.

  19. 基于空间碎片环境的导弹空间飞行安全分析%Security Analysis about Long-Range Ballistic Missile Flying in the Environment of Space Debris

    Institute of Scientific and Technical Information of China (English)

    王剑; 谭守林; 雷刚

    2013-01-01

    针对导弹空间飞行环境的日益恶化,为了分析空间碎片对远程弹道导弹空间飞行安全的影响,分析了导弹弹道和空间碎片预测模型,建立了基于数值法的远程弹道导弹与空间碎片碰撞预警模型,通过仿真分析了空间碎片对远程弹道导弹飞行安全的影响.仿真结果表明,空间碎片对远程弹道导弹空间飞行安全具有潜在的威胁,研究结果可为导弹飞行安全预警和导弹发射窗口选择提供一些借鉴.%As the flying space environment has become deteriorated, according to the analysis of missile's trajectory and space debris' forecast model, a model of impact alert between long-range ballistic missile and space debris is established. The security influence for long-range ballistic missile from space debris is analyzed according to simulation. The simulation results indicate that there is underlying threatening to the long-range ballistic missile, and the research results can be used in flying security alert and selecting launch windows of missile.

  20. A New Algorithm with Variable-Structure Multiple Model for Tracking Ballistic Missile at Entire Flight Stages%跟踪弹道导弹全阶段的可变多模型方法

    Institute of Scientific and Technical Information of China (English)

    钮俊清; 单奇; 任清安; 刘军伟

    2011-01-01

    弹道导弹跟踪是弹道导弹防御系统中最核心的问题,然而传统的基于单运动模型的跟踪方法不能适用于跟踪弹道导弹的所有阶段。提出一种新的可变多模型(VUF)的跟踪方法,该方法具有以下的优势:采用多模型的结构,适用于跟踪任意阶段的弹道导弹;可变模型集的特征有效地提高了精度,同时降低了计算复杂度;采用UKF滤波方法具有更好的跟踪精度。仿真实验中设计了三个实验场景,与传统的EKF算法相比该方法明显地提高了跟踪的精度。特别是在弹道目标飞行阶段转换时,具有一定的识别能力和更鲁棒的跟踪性能。%In missile defense system, tracking ballistic target is the most key problem. However, the traditional method based on single-state model is not suitable for tracking ballistic target at all flight stages. The paper addresses a new tracking algorithm with variable-structure multiple model. It has several advantages. It is capable of tracking ballistic target at entire flight stages due to multiple model. Based on variable-structure, it improves tracking precision effectively and makes computational complexity lower. It has better tracking precision by using unscented Kalman filtering. Three simulation scenarios had been designed. Compared to the traditional EKF algorithm it has better estimation performance. Especially, it has some identification ability and more robust tracking performance during the switch phase of ballistic target.

  1. Advanced Missile Signature Center

    Data.gov (United States)

    Federal Laboratory Consortium — The Advanced Missile Signature Center (AMSC) is a national facility supporting the Missile Defense Agency (MDA) and other DoD programs and customers with analysis,...

  2. 浅述美国海军防空反导雷达的发展%Development of Air and Missile Defense Radar for US Navy

    Institute of Scientific and Technical Information of China (English)

    谢勇光

    2011-01-01

    美国海军防空反导雷达(AMDR)是一种正在研发的新型固态有源相控阵雷达.AMDR集成S波段和X波段雷达的优异性能,可用雷达套件控制器协调各套件同时工作,并能使未来战舰能够检测和跟踪多种威胁,包括弹道导弹、战机、超音速以及掠海反舰导弹.AMDR具有开放式体系结构和灵活的升级能力,可部署于不同舰船平台,是美海军未来40年主要的雷达系统.文中首先对AMDR系统做了一个简单的介绍;然后,对其设计特点进行了详细的分析,包括存在的主要问题,并对该系统的作战能力做了说明;最后,将此系统与其他系统做了对比分析.%US navy air and missile defense radar ( AMDR) is a developing new solid-state active phased array radar( APAR) , which integrates superior performance of both S band and X band radars under control of radar suite controller, providing future ship with an ability to detect and track various theaters, including ballistic missile, fighter aircraft, supersonic and sea-skimming anti-ship missile. It is given open architecture and flexible scalable capability, available to be deployed on diverse platforms, promising the premier radar system for US navy in the future 40 years. Firstly, AMDR radar system is introduced briefly in this paper. After that, the design features are analysed in details, including existing problems, meanwhile, introduced combatant capability of the system is introduced in this part. Finally, the radar system is compared with other radar systems.

  3. Determining the Probability of Violating Upper-Level Wind Constraints for the Launch of Minuteman Ill Ballistic Missiles At Vandenberg Air Force Base

    Science.gov (United States)

    Shafer, Jaclyn A.; Brock, Tyler M.

    2013-01-01

    The 30th Operational Support Squadron Weather Flight (30 OSSWF) provides comprehensive weather services to the space program at Vandenberg Air Force Base (VAFB) in California. One of their responsibilities is to monitor upper-level winds to ensure safe launch operations of the Minuteman Ill ballistic missile. The 30 OSSWF requested the Applied Meteorology Unit (AMU) analyze VAFB sounding data to determine the probability of violating (PoV) upper-level thresholds for wind speed and shear constraints specific to this launch vehicle, and to develop a graphical user interface (GUI) that will calculate the PoV of each constraint on the day of launch. The AMU suggested also including forecast sounding data from the Rapid Refresh (RAP) model. This would provide further insight for the launch weather officers (LWOs) when determining if a wind constraint violation will occur over the next few hours, and help to improve the overall upper winds forecast on launch day.

  4. Suppression of Elastic Vibration for Air Defense Missile%防空导弹弹性振动抑制

    Institute of Scientific and Technical Information of China (English)

    许龙; 余祖铸

    2011-01-01

    基于防空导弹的数学模型,根据弹体弹性振动的特性,对抑制其振动的方法和稳定回路设计进行了研究。通过确定频带宽度稳定刚性弹体的姿态运动,采用陷波补偿相位稳定和增益稳定抑制弹性振动以稳定弹性弹体。给出了稳定回路的设计,并比较了不同方法的特点。%According to the characteristics of the elastic vibration of the air defense missile's body,the method to suppress the vibration and the design of the stabilizing loop were studied based on the mathematic model of the missile in this paper.The attitude of the rigid body of the missile was stabilized through determining the frequency width.The elastic body of the missile was stabilized through notch compensation phase and gain stabilization to suppress the elastic vibration.The design of the stabilization loop was given out.The characteristics of different ways were compared.

  5. 弹道导弹SINS/CNS 组合导航系统建模与性能仿真%System Modeling and Performance Simulation on SINS/CNS Integrated Navigation System for Ballistic Missile

    Institute of Scientific and Technical Information of China (English)

    王鑫; 王新龙

    2015-01-01

    Combined with the characteristics of ballistic missile and the model error caused by uncer-tain noise characteristics in engineering practice, this paper proposes a SINS/CNS integrated navigation system suitable for ballistic missiles.This system, integrated some characteristics of simple combination models and overall optimal correction combination models, uses the adaptive Kalman filtering to ensure the stability and robustness of the filter.In the simulation, according to the missile trajectory, it establi-shes a reasonable, complete guide star catalog of missile.The simulation illustrates that this navigation scheme can improve the precision of navigation parameters of ballistic missile.%针对弹道导弹在工程实际中噪声特性的不确定性及其引起的模型误差,本文提出了一种适用于弹道导弹的 SINS/CNS 组合导航方案。该方案融合了简单组合模式和基于全面最优校正的组合模式特点,采用自适应卡尔曼滤波来保证滤波的稳定性和鲁棒性,并根据导弹的飞行弹道,建立了合理、完备的弹载导航星表。仿真验证结果表明,该导航方案可以达到全面提高弹道导弹导航参数精度的目的。

  6. Predictive Guidance of Intercepting Tactical Ballistic Missile in Boost Phase%战术弹道导弹助推段拦截预测导引方法

    Institute of Scientific and Technical Information of China (English)

    孙宏云; 董敏周; 于云峰

    2011-01-01

    针对弹道导弹助推段拦截的末制导问题进行研究,建立了弹道导弹助推段的运动模型,根据助推段的运动特点提出了预测导引末制导方法,通过分析零效脱靶量将比例导引的过载指令与轨控发动机工作时间进行等效.在不同的弹目速度初始夹角下分别用预测导引和比例导引法仿真并进行对比分析,仿真结果表明预测导引较比例导引在较大的末制导起始区域内具有更短的拦截时间和更少的轨控发动机燃料消耗量.%Focused on the terminal guidance law of intercepting tactical ballistic missile in boost phase, the motion model of TBM' boost-phase is established.Touse the predictive guidance as the terminal guidance law is put forward.By analyzing the zero-effort-miss, change the proportional navigation guidance (PN) command to the rail engine' working time.Separately simulated the intercepting scene with predictive guidance and PN at different initial missile velocity angle, and compared the results.The simulation results show that the predictive guidance has less intercepting time need less rail engine' working time than the PN with large terminal guidance initial area.

  7. 一种基于双预警卫星的弹道导弹轨迹重建算法%Algorithm of reconstruction for ballistic missile trajectory based on double early warning satellites

    Institute of Scientific and Technical Information of China (English)

    王树文; 姜海林; 胡沛

    2015-01-01

    In view of the complexity of the reconstruction algorithm for early warning satellite to ballistic missile, and the trade-off between high precision and real-time being hard, we propose a reconstruction algorithm of ballistic missile flight path based on observation of the geo-stationary earth orbit (GEO) double early warning satellites, by employing the conditions of epipolar constraint and time constraint in stereo vision matching, and perform a simulation experiment. Simulation results illustrate that the reconstruction trajectory of the ballistic missile’s powered phase comes close to the real one, the distance error between the reconstruction point and the real one is less than 2 km under the circumstance of camera detection error being small, which can meet the demand of the following estimation of ballistic missile launching point and forecast of drop point.%针对预警卫星对弹道导弹轨迹重建算法复杂、高精度与实时性难以兼顾的问题,利用立体视觉匹配中的目标点外极线约束及时间约束条件,提出了一种基于地球静止轨道(GEO)双预警卫星观测的弹道导弹飞行轨迹重建算法,并进行了仿真实验。实验结果表明,该算法对弹道导弹主动段重建轨迹与真实轨迹接近,在相机检测误差较小情况下重建点距离真实点误差小于2 km,可满足后续对弹道导弹进行发射点估计及落点预报需求。

  8. 主动段终点参数对弹道导弹射程的影响研究%The Influence of Termination Point Parameters on Ballistic Missile Range

    Institute of Scientific and Technical Information of China (English)

    王瑞臣; 洪贞启; 李建林

    2011-01-01

    主动段终点参数直接影响弹道导弹的战术技术指标实现与否.通过简化弹道导弹的飞行弹道模型,分析计算了主动段终点参数对弹道导弹射程及落点精度的影响大小.在导弹武器系统作战使用过程中应注意把握,尽量减小干扰因素对弹道导弹主动段终点参数的影响.%Whether the tactical technique index of ballistic missile is reached is affected by the parameters of powered-flight phase termination point. The trajectory model is set up in this paper, and the influence of terminition point parameters on range and accuracy is analyzed. The influence of some factors on ballistic missile accuracy should be reduced in the process of operation of missile weapon system.

  9. 天波超视距雷达探测弹道导弹性能研究磁%Study of Detection Performance of Skywave OTHR on Ballistic Missile

    Institute of Scientific and Technical Information of China (English)

    刘诗华; 李德芳; 申正义

    2015-01-01

    研究了天波雷达探测对弹道导弹的探测性能。研究从天波雷达探测火箭的机理和方式入手,分析了基于箭体、尾焰和人工电离层洞等三种探测方式。从雷达截面积(RCS )的角度对天波雷达探测弹道导弹和隐身飞机的性能进行了比较。最后,基于天波雷达探测火箭的方式,研究了天波雷达探测潜射弹道导弹的探测性能。%The detection performance of skywave OTHR on ballistic missile is studied .The study is based on the detec‐tion mechanism and methods of skywave OTHR on rocket .The three detection methods ,which based on rocket body ,plume and artificial ionosphere hole ,are analyzed .As viewed from the RCS ,the detection performance of skywave OTHR on bal‐listic missile is compared to the performance of skywave OTHR on stealth aircraft .Finally ,based on the methods of skywave OTHR on rocket ,the detection performance of skywave OTHR on ballistic missile is researched .

  10. 适用于弹道导弹的导航星选取方法%Guide star selection method applied to ballistic missile

    Institute of Scientific and Technical Information of China (English)

    王宏力; 陈聪; 崔祥祥; 姜伟

    2013-01-01

    The present researches on guide star selection methods applied to ballistic missile are not e-nough, therefore a novel uniformization selection method according to standard trajectory was discussed. By analyzing the impacts of missile trajectory and various flight parameters, and constructing the ' pseudo celestial sphere coordinate frame' , the guide star selection region was determined. The problems caused by fire direction changing or coordinates boundary exceeding were simplified. The guide stars were selected and homogenized on basis of reference points on celestial sphere and the proposed ' Separation-Magnitude ' weighting method. The on-board guide star catalog having better applicability was generated via k-vector index approach, and the efficiency of star identification algorithm would be improved. The simulation results indicate that the method implements simply. Much less guide stars which have better uniform distribution are selected. The elapsed time of star identification is effectively reduced on the basis of the undiminished identification success rate.%针对当前适用于弹道导弹的导航星选取方法较少,研究了一种根据标准弹道均匀化选取导航星的方法.通过分析导弹飞行弹道及飞行参数的影响,在构建“伪天球”坐标系的基础上,确定了导航星的选取区域,简化了因射向变化、坐标越界等造成计算和搜索比较复杂的问题;基于天球上的基准点及提出的“距离-星等”加权法,均匀化地筛选导航星,并按照k-vector索引方式构建适用性较好的弹载导航星表,可以有效地提高星图识别算法的效率.仿真结果表明,该方法简单易行,选取的导航星数量少,分布均匀性好,在不降低星图识别成功率的基础上,能够有效地减少识别时间.

  11. Toward Armageddon: The proliferation of unconventional weapons and ballistic missiles in the Middle East. Occasional Paper No. 36

    Energy Technology Data Exchange (ETDEWEB)

    Miller, A.J.

    1989-12-01

    The author concludes that it is probable that unconventional weapons and their associated delivery systems will form a permanent part of future political and strategic calculations in the Middle East. Some possible consequences of this situation can be divided into three classes: intra-regional, inter-regional and extra-regional. There is no doubt that Israel, driven by the need for security,precipitated the proliferation of unconventional weapons and of surface-to-surface missiles in the Middle East. It will now be driven to secure itself from the new threat to its security posed by its regional opponents. The most significant extra-regional consequence of developments in the Middle East may be further complication of great power arms control negotiations. To the re-discovery by the United States and the Soviet Union of their obligations under the Non-Proliferation Treaty to reduce the level of their nuclear weapons must now be added the desire to reduce, if not entirely eliminate, their chemical weapons stockpiles in advance of a global ban. It is possible that lesser powers will learn from the evidence of the great powers behavior, although that contradicts much of what we know of the psychology of decision making in international politics. What is necessary, though not necessarily sufficient, is that the U.S. and the USSR as the two external powers with potentially the greatest leverage, work together toward the resolution of the underlying causes of conflict in a region marked by more than a generation of competition between them.

  12. Target Recognition for Ballistic Missile Based on Dynamic RCS Time Series%基于RCS序列的助推段弹道导弹识别

    Institute of Scientific and Technical Information of China (English)

    隋栋训; 童创明; 王童; 王伟杰

    2016-01-01

    在弹道导弹的助推段,通过低分辨率雷达得到RCS序列作为识别的重要信息。由于运动特性和电磁散射特性的差异,弹道导弹在助推段的RCS序列与其他目标相比具有可识别性,但需要对其RCS序列进行处理。基于目标识别技术,详细阐述能从RCS序列中提取出的特征参数,并通过直方图、N点截图等方法给出了直观的反映。最后,将弹道导弹助推段特征与飞机、燃料舱等典型目标进行对比,得到可以作为识别参量的特征参数,并通过类内类间距离验证了有效性。%Information obtained by dynamic RCS time series of low-resolution narrowband radar is very helpful to radar target identification,especially to ballistic missile on boost phase. Because of the difference of kinetic and electromagnetic scattering characters,the RCS time series can be recognized from other target. It’s necessary to extract the feature on the boost phase.The method on the technology of target recognition is discussed in detail,and the feature is also showed by N point reduction and column plot. At last,compared with fighter and fuel compartment,typical characteristic parameter is got,and the effectiveness is tested and verified by between-class and within-class distance.

  13. Missile defence : An overview

    NARCIS (Netherlands)

    Weimar, P.W.L.

    2012-01-01

    At the present day, an unparalleled number of international actors, be it national governments or non-state groups, have acquired or are seeking to acquire both weapons of mass destruction and the means to deliver them. Those means of delivery can be Ballistic Missiles that can bridge vast – even in

  14. 舰载弹炮结合近程武器系统技术研究%Study on Shipped Missile-Gun Integrated Defense Weapon System

    Institute of Scientific and Technical Information of China (English)

    白奕

    2014-01-01

    现代高性能反舰导弹是舰艇末端防御的最大威胁,而舰载弹炮结合近程武器系统为舰艇的末端防御提供了一种有效的途径。分析了舰载弹炮结合近程武器系统的作战使用和主要特点,针对海上空袭武器的特点,重点研究了增强系统抗饱和攻击能力的设计方法,并探讨了舰载弹炮结合近程武器系统在现代海战中的使用方向。%Modern high-powered antiship missile is the main threaten of ship,and shipped missile-gun integrated defense weapon system is an effective way to the terminal defense of ship. This paper first analyzes the combat operation and main characteristic of missile-gun integrated defense weapon system,then studies the key factor of designing a system. At last the system usage is discussed in the modern sea war.

  15. Determining the Probability of Violating Upper-Level Wind Constraints for the Launch of Minuteman III Ballistic Missiles at Vandenberg Air Force Base

    Science.gov (United States)

    Shafer, Jaclyn A.; Brock, Tyler M.

    2012-01-01

    The 30th Operational Support Squadron Weather Flight (30 OSSWF) provides comprehensive weather services to the space program at Vandenberg Air Force Base (VAFB) in California. One of their responsibilities is to monitor upper-level winds to ensure safe launch operations of the Minuteman Ill ballistic missile. The 30 OSSWF tasked the Applied Meteorology Unit (AMU) to analyze VAFB sounding data with the goal of determining the probability of violating (PoV) their upper-level thresholds for wind speed and shear constraints specific to this launch vehicle, and to develop a tool that will calculate the PoV of each constraint on the day of launch. In order to calculate the probability of exceeding each constraint, the AMU collected and analyzed historical data from VAFB. The historical sounding data were retrieved from the National Oceanic and Atmospheric Administration Earth System Research Laboratory archive for the years 1994-2011 and then stratified into four sub-seasons: January-March, April-June, July-September, and October-December. The AMU determined the theoretical distributions that best fit the maximum wind speed and maximum wind shear datasets and applied this information when calculating the averages and standard deviations needed for the historical and real-time PoV calculations. In addition, the AMU included forecast sounding data from the Rapid Refresh model. This information provides further insight for the launch weather officers (LWOs) when determining if a wind constraint violation will occur over the next few hours on the day of launch. The AMU developed an interactive graphical user interface (GUI) in Microsoft Excel using Visual Basic for Applications. The GUI displays the critical sounding data easily and quickly for LWOs on day of launch. This tool will replace the existing one used by the 30 OSSWF, assist the LWOs in determining the probability of exceeding specific wind threshold values, and help to improve the overall upper winds forecast for

  16. Interior Ballistic Modeling and Simulation of Underwater Launched Missile Using Concentric Canister Launcher%同心筒水下发射内弹道建模与仿真研究

    Institute of Scientific and Technical Information of China (English)

    袁绪龙; 王亚东; 刘维

    2013-01-01

    To construct a fast calculation method of interior ballistics of underwater launched missile using Concentric Canister Launcher(CCL),a simulation model of CCL was established according to the first law of thermodynamics,and power characteristics and underwater environment were considered.The empirical parameters in this model were decided using CFD solutions,and they were verified by more calculations.The influences of design parameters on the interior ballistics were studied by the verified model.The simulation shows that the sizes of canister top and bottom restricting parts can be used to adjust launching velocity of missile;the size of canister bottom restricting part can be adapted to modify the acceleration of missile.It can increase the adjusting range of velocity to increase initial volumes of inner and outer canister.The simulation method and results offer reference for engineers.%为构建一种快速的同心筒水下发射内弹道算法,采用热力学第一定律,结合导弹动力装置特性及水下环境需求,建立了同心筒水下发射内弹道计算模型,用CFD结果辨识并校验模型经验参数.应用校验的模型研究了发射装置设计参数对内弹道参数的影响规律.结果表明:筒口、筒底限流尺寸均可用于调速,筒底限流尺寸可用于调节过载,内、外筒初始容积增大可增大调速范围.仿真方法和结果可供工程设计人员参考.

  17. 基于导弹空间飞行的空间碎片筛选方法研究%Analysis of Filtration Methods for Space Debris Based on Impacting Alert When Long-distance Ballistic Missile Flying in Space

    Institute of Scientific and Technical Information of China (English)

    王剑; 谭守林; 杨晓云; 牛国华

    2012-01-01

    随着空间活动的日益频繁,空间碎片的数量也与日俱增,给远程弹道导弹的空间飞行安全带来巨大威胁.针对空间碎片数目繁多,为了快速进行导弹空间飞行安全预警和发射窗口选择,根据远程弹道导弹空间飞行特点,提出了适用于导弹与空间碎片碰撞预警的空间碎片筛选方法,并通过仿真计算证明了该筛选方法的科学性和合理性,该筛选方法可提高导弹空间飞行安全预警效率并缩短预警时间.%Seeing that the space environment in which missiles flies has increasingly deteriorated, and the large threat has been worked by space debris. When the impacting alert between long-distance ballistic missile and space debris being researched, the amount of debris is very huge and it is impossible to tack place impacts between missile and some debris, so it is necessary to filtrate space debris before impacting alert. According to the characters of flying of missile, the filtration methods for space debris are given, and the rationality and validity of those methods were proved by simulation and calculation. Those methods can improve alert efficiency and cut alert time.

  18. 基于Multi-Agent的防空导弹武器系统模型设计%Design of Multi-Agent Based Model on Air Defense Missile Weapon System

    Institute of Scientific and Technical Information of China (English)

    陈宝印; 栾立秋; 张成斌

    2011-01-01

    建立科学的结构模型是进行防空导弹武器系统仿真的基础和关键环节.针对防空导弹武器系统的特点,提出了基于Multi-Agent的防空导弹武器系统模型建模方法,设计了防空导弹武器系统模型结构.利用Multi-Agent建模技术,把防空导弹武器系统实体映射成相应的Multi-Agent系统,并以Agent的形式对防空导弹武器系统这一客观复杂系统进行了深刻的认识,为防空导弹武器系统建模仿真奠定了基础.%Forming a scientific system model is the key of Air Defense Missile Weapon System simulation. According to the characters of Air Defense Missile Weapon System, a modeling method of multi-agent based model on Air Defense Missile Weapon System is given. The framework on Air Defense Missile Weapon System is designed. Using the Multi-Agent modeling technology, maps the Air Defense Missile Weapon System entity the corresponding Multi-Agent system, and carries on the profound understanding by the Agent form to Air Defense Missile Weapon System this objective complicated, which will be helpful to realize the modeling simulation on Air Defense Missile Weapon System.

  19. Tornado missile transport analysis

    International Nuclear Information System (INIS)

    A methodology has been developed to simulate the initial release conditions and subsequent motion of objects transported by tornadoes. A probabilistic three-degree-of-freedom trajectory model which includes drag, lift, and side forces has been developed to simulate rigid body dynamics in turbulent tornado flow fields. Comparisons of this random orientation model to results from ballistic three-degree-of-freedom trajectory analysis are presented and the results suggest that the simpler models are potentially unconservative in predicting missile range and impact velocity. A missile injection methodology has also been developed which treats injection as the composite of all missile interactions in the near-ground domain and relies on a restraint force exceedance criterion to initialize missile release relative to the translating tornado. The aerodynamic forces acting on a potential missile during injection suggest a multi-peaked time history which is significantly influenced by missile offset position from the vortex center. A simulation study of missile injection has been performed to determine a conservative range for the assumed horizontal restraining force. (Auth.)

  20. A Calculation Method of Burst Height of Ballistic Missile Based on Radar Seeker%一种基于雷达导引头的弹道导弹爆高解算方法

    Institute of Scientific and Technical Information of China (English)

    郑宗贵; 王继平; 林红斌; 解静

    2014-01-01

    目前弹道导弹主要通过无线电引信测高来进行战斗部爆高控制,但弹头的再入环境对无线电引信测高装置的要求非常高,且引信存在着易被干扰的问题。为此,该文针对采用雷达景象匹配末制导的弹道导弹,提出一种基于雷达导引头的弹道导弹爆高控制方法,通过雷达导引头测高数据与惯性导航数据的融合处理,实时计算弹头飞行高程,来实现爆高控制,既保证了精度,又增强了抗干扰能力。仿真算例证明了该方法的有效性和爆高解算精度。%At present the height of the warhead of ballistic missile is measured by the radio fuze for the burst height control of the warhead, but the reentry environment of the warhead has very high requirement for the measure set of the radio fuze, and there exists the issue of the radio fuze to be jammed. In the paper, for the ballistic missile adopting the radar scene matching terminal guidance, a calculation method of burst height of ballistic missile based on radar seeker is put forward, by fusing the height measure data of the scene matching radar seeker and the inertial navigation data, the height of the warhead is calculated in real time to realize the burst height control, which ensures the precision and improves anti-jamming capability. The validity of the method and the calculation precision of the burst height are proved by simulation and calculation.

  1. 一种新的最优空基反弹道导弹中制导方法研究%Study on a New Air-Based Intercepting Ballistic Missile Midcourse Guidance Method

    Institute of Scientific and Technical Information of China (English)

    刘浩敏

    2015-01-01

    The air-based anti-missile method has been drawn high value by many great military pow-ers in the world for its flexible deployment and quick reaction .It is extremely important to design a pre-cise and energy optimal midcourse guidance law for the interceptor considering the advantages to intercept the ballistic missiles in the midcourse according to some common planned trajectory .Firstly, this thesis designs a new midcourse guidance law for air-based intercepting ballistic missile based on LQR theory by using a simplified relative kinematic model of “Interceptor-Target”, then the new guidance law is verified by digital simulation with the initial condition of the “Interceptor-Target”.The results show that the new designed midcourse guidance law could meet the requirement of the midcourse guidance properly in an air -based anti-missile system .%空基反导以其部署灵活、响应速度快等特点而受到各军事大国高度重视。针对常见的规划弹道,对处于飞行中段的弹道导弹进行拦截具有诸多优势,因此,为拦截器设计一种精确、能耗最优的中制导律至关重要。首先,本文基于简化的弹-目相对运动学模型,运用LQR理论设计了一种新的能量最优空基反弹道导弹中制导律;其次,根据给定的弹-目初始条件,通过数字仿真对所设计的制导律进行了验证。结果表明,本文提出的制导律可以较好地满足空基拦截弹道导弹中制导要求。

  2. 弹道导弹总体参数的混合遗传算法全局优化%Hybrid genetic algorithm global optimization of configuration design for ballistic missiles

    Institute of Scientific and Technical Information of China (English)

    陈江宁; 王和平

    2011-01-01

    液体火箭发动机推进弹道式导弹总体设计参数的全局最优化问题是亟待解决的计算问题.遗传算法具有全局搜索能力强、鲁棒性强、适于并行处理的特点,而Powell算法具有很好的求解局部最优解的能力.将两种方法进行有效改进后使之相结合,设计出并行全局最优化混合遗传算法.并以此为基础,建立了液体火箭发动机推进弹道式导弹总体优化设计模型.以液体火箭发动机推进弹道式导弹的起飞质量最小为目标,对液体推进剂弹道式导弹设计参数进行了优化设计.数值优化结果表明:该混合算法提高了搜索全局最优解的速度,优化精度高,且避免了初值敏感、病态梯度和局部收敛等问题,能够搜索到全局最优设计参数.%The matters of global optimization of configuration design for liquid rocket engine propelled ballistic missiles were in dire need of computation. Genetic algorithms have the characters such as strong ability in find global optimal solution, strong robustness, and good parallel efficiency, while Powell algorithm had very strong ability to find the locally optimal solution. In this paper, two methods after some efficient improvement were combined,and a parallel global optimization hybrid genetic algorithm was designed. A numerical optimization model for liquid rocket engine propelled ballistic missiles is developed based on the hybrid genetic algorithm. Take-off weight of liquid rocket engine propelled missiles was taken as the objective function and the design parameters for liquid rocket engine propelled missiles as optimization design variables. The numerical optimization results show that this hybrid algorithm could efficiently get the globally optimal solution and take on high optimization precision. Moreover, it avoids many shortcomings, such as initial value sensitivity, ill-conditioned gradient and local convergence, and so on. It can obtain global optimum design

  3. The Trend of Missile-Gun Combined Weapon System for Aerial Defense%弹炮结合防空武器系统新趋势

    Institute of Scientific and Technical Information of China (English)

    陈薇; 王军

    2016-01-01

    Since the Kosovo War started to use a form of simple air raids and counter-air raids,a increasing number of wars use air raids to attack the enemy,so how to defense the enemy in the air become more and more important. Missile-Gun combined weapon system not only has a big air defense area but also has a high effective-cost,so it will become the trend of air defense weapon system. This paper describes the structure and classification of Missile-Gun combined weapon system,and analyzes the advantages and disadvantages of the current systems; finally the trend of Missile-Gun combined weapon system is proposed.%自从科索沃战争开创了单纯空袭作战与反空袭作战的先例之后,空袭就成为了战争的焦点,如何更好地抵御空中目标的来袭成为各国战争防御的主题。弹炮结合防空武器系统具有防空区域大、效费比高等优点,是防空武器系统的发展趋势之一。在分析现有典型弹炮结合防空武器系统的基础上,依据弹炮结合武器系统是否共用火控系统将其分为弹炮混编式和弹炮同控式两种形式;随后,结合现代空袭的特点提出了弹炮结合武器系统的发展趋势。

  4. 一种用于弹道导弹助推段拦截的最优制导律%An Optimal Guidance Law for Boost Phase Interception of Ballistic Missile

    Institute of Scientific and Technical Information of China (English)

    肖增博; 雷虎民; 叶继坤; 宋龙; 徐剑芸

    2011-01-01

    In order to intercept ballistic missile during the boost phase,the linear quadratic differential game theory was introduced to design air-borne interceptor guidance law.Based on the pursuit-evasion conflict model between interceptor and ballistic missile,two optimal guidance commands were proposed separately with previous target information and without.The guidance process was divided to the terminal guidance phase and the trajectory-shaping phase by applying the control decomposition strategy.The proposed guidance law can eliminate the effects of target evasive maneuver and estimation error,and the guidance law has strong applicability.The simulation results show that the guidance laws satisfy the required index,and the interceptor can hit the target directly.%针对弹道导弹助推段的拦截问题,基于线性二次型微分对策理论,提出了空基拦截弹直接碰撞制导律.根据拦截弹和弹道目标的追逃对策模型,在具有目标先验信息和无目标先验信息条件下分别设计了拦截弹最优制导指令;通过控制指令分解,将拦截弹制导过程分为弹道形成制导段和末制导段.该制导律可以消除目标机动和估计误差带来的影响,具有较强的适应性.仿真结果表明,所设计的制导律满足设计指标,达到了直接碰撞杀伤目标的目的.

  5. 平流层飞艇高能激光武器防御弹道导弹%Defending Ballistic Missile using High-Energy Laser Weapon basing Stratosphere Airships

    Institute of Scientific and Technical Information of China (English)

    车学科; 聂万胜; 何炬恒

    2011-01-01

    防御弹道导弹逐渐受到世界各国的重视,扩大拦截窗口是重要的发展趋势之一.平流层飞艇有可能通过艇载激光武器或者中继反射地基激光两种方式拦截自由段弹道导弹,为评估这两种方式的拦截效果和可行性,分析了平流层飞艇搭载高能激光武器的可能性以及中继反射作战方式的特点,建立了激光烧蚀模型,采用数值计算方法对激光的烧蚀效果进行了研究.结果表明:平流层飞艇部署位置应距离导弹发射点800~1000km,平流层中继激光飞艇能够在短时间内引爆弹头,艇载激光武器采用烧蚀弹头防热层的方法同样可以达到拦截弹道导弹的目的.%The importance of ballistic missile defence is known by many countries. One main trend is extending the intercept window. Stratosphere airships can intercept ballistic missile through two ways of airship borne laser and relay ground base laser. In order to evaluate the intercept capability and feasibility of these ways, the possibility that stratosphere airship can bear high-energy laser weapon and the superiority of relay mode are analyzed in this paper, and the laser ablation model is built, furthermore the laser ablation effect is computed. The results show airship should deploy 800~1000km away form the missile launch point, and the laser-relay airship will detonate warhead rapidly, while airship bome laser can achieve same interception effect by ablating the thermal protection layer.

  6. A coordination policy for the NATO SEASPARROW Missile and the Rolling Airframe Missile using dynamic programming

    OpenAIRE

    Drennan, Arthur Paul

    1994-01-01

    This thesis develops a dynamic program, the SEASPARROW Coordinated Assignment Model (SCAM), that determines the optimal coordinated assignment policy for the SEASPARROW missile in a shipboard self defense weapon configuration consisting of the NATO SEASPARROW Missile System, the Rolling Airframe Missile and the Phalanx Close-In Weapon System. Threat scenarios are described by the type of' anti-ship cruise missile, the number of threat missiles, the total duration of the arrival window and the...

  7. Ballistic injury.

    Science.gov (United States)

    Fackler, M L

    1986-12-01

    Wound profiles made under controlled conditions in the wound ballistics laboratory at the Letterman Army Institute of Research showed the location along their tissue path at which projectiles cause tissue disruption and the type of disruption (crush from direct contact with the projectile or stretch from temporary cavitation). Comparison of wound profiles showed the fallacy in attempting to judge wound severity using velocity alone, and laid to rest the common belief that in treating a wound caused by a high-velocity missile, one needs to excise tissue far in excess of that which appears damaged. All penetrating projectile wounds, whether civilian or military, therefore should be treated the same regardless of projectile velocity. Diagnosis of the approximate amount and location of tissue disruption is made by physical examination and appropriate radiographic studies. These wounds are contaminated, and coverage with a penicillin-type antibiotic should be provided. PMID:3777618

  8. Missile Electro-Optical Countermeasures Simulation Laboratory

    Data.gov (United States)

    Federal Laboratory Consortium — This laboratory comprises several hardware-in-the-loop missile flight simulations designed specifically to evaluate the effectiveness of electro-optical air defense...

  9. 基于DoDAF的舰载弹炮结合防空武器系统模型%Shipboard Missile Gun Integrated Air-Defense Weapon System Model Based on DoDAF

    Institute of Scientific and Technical Information of China (English)

    王洪胜; 禹大勇; 曲延明

    2014-01-01

    In current sea battle, aiming at the point-defense ship-to-air missile and small caliber shipboard artillery can’t realize reserving battle task independently, establish shipboard missile-gun integrated air-defense weapon system based on DoDAF. Analyze design process of shipboard missile-gun integrated air-defense weapon system, combining with military requirement and battle flow to establish part of battle model, then describe operation process of shipboard missile-gun integrated air-defense weapon system in water surface ship terminal defense. It promotes the top layer design of shipboard missile-gun integrated air-defense weapon system and gives technology support for danger control.%针对现代海战中点防御舰空导弹和小口径舰炮难以独立完成预定作战任务的问题,构建一种基于DoDAF的舰载弹炮结合防空武器系统模型。分析了舰载弹炮结合防空武器系统设计步骤,结合军事需求、作战流程构建了部分作战模型,并阐述了舰载弹炮结合防空武器系统在水面舰艇末端防御作战中的活动过程。目的是推动舰载弹炮结合防空武器系统顶层设计和风险控制提供技术支撑。

  10. Missile autopilot design using Mu-Synthesis

    OpenAIRE

    Bibel, John Eugene

    1998-01-01

    Due to increasingly difficult threats, current air defense missile systems are pushed to the limits of their performance capabilities. In order to defend against these more stressing threats, interceptor missiles require greater maneuverability, faster response time, and increased robustness to more severe environmental conditions. One of the most critical missile system elements is the flight control system, since its time constant is typically half of the total missile system time constant....

  11. Research into Passive Jamming Covering Terminal Penetration of Ballistic Missile%无源干扰掩护弹道导弹末段突防研究

    Institute of Scientific and Technical Information of China (English)

    田志峰; 齐锋; 欧阳科举

    2011-01-01

    Through analyzing the signal reflection characteristics of passive antenna array and the time resource consumption rate, tracking and intercept rate, etc. of land-based low altitude antimissile system, this paper educes the formula using passive antenna array as a heavy decoy to perform passive jamming to the anti-missile system, based on which, proves the effect of passive antenna array jaming anti-missile system through the calculation result of an example.%通过分析无源天线阵的信号反射特性和陆基低空反导系统的时间资源占用率、跟踪拦截率等,得出了运用无源天线阵充当重诱饵对反导系统实施无源干扰的公式,在此基础上,通过实例的计算结果,验证了无源天线阵对反导系统的干扰效果。

  12. REALIZATION OF GPS/SST/SINS INTEGRATED NAVIGATION FILTER ALGORITHM FOR BALLISTIC MISSILE%用于弹道导弹的GPS/SST/SINS组合导航滤波算法实现

    Institute of Scientific and Technical Information of China (English)

    康国华; 刘建业; 祝燕华; 熊智

    2005-01-01

    Considering the domestic single navigation system of the ballistic missile, a new filter method is presented. The method integrates the information of the strapdown star tracker (SST) attitude, the position and the velocity of a high speed GPS with a strapdown inertial navigation system (SINS) information into one filter, thus improving the precision of the attitude, the velocity, and the position. Finally, the GPS/SST/SINS simulation platform is designed. Simulation results demonstrate that the filter is robust and reliable, and the precision rises to the comparative level abroad.%针对目前国内弹道导弹导航系统单一的情况,文中提出一种滤波算法.该算法将捷联星光跟踪仪(Strapdown star tracker, SST)的姿态信息、高速GPS的位置、速度信息与捷联惯导进行组合滤波,全面提高了导航的姿态、速度和位置精度.最后以该算法为核心,设计并实现了用于弹道导弹的GPS/SST/SINS组合导航系统实时仿真平台.仿真结果表明,该滤波算法稳定可靠,系统精度达到国外同等水平.

  13. 机动发射的弹道导弹飞行诸元的快速计算%A rapid method for flight program design of the ballistic missile launched on mobile platform

    Institute of Scientific and Technical Information of China (English)

    韦文书; 荆武兴; 高长生

    2012-01-01

    基于解析预报与数值寻优相结合的方法,本文研究机动发射的弹道导弹飞行诸元快速设计问题.首先,利用线性回归方法建立了导弹诸参数与发射信息之间的多项式拟合关系式,利用该式可以得到飞行方案诸参数迭代初值;然后,以弹道落点纵向偏差、横向偏差及弹道顶点高度偏差平方和极小为指标函数,采用Levenberg—Marquardt方法搜索诸参数精确解;最后,以民兵Ⅲ弹道导弹为例,对所提方法进行了仿真验证,研究结果表明,该方法计算量少,适合已定参数的导弹大范围机动发射的快速计算,且在落点精度要求不高的情况下,可以用解析表达式的解作为弹道飞行方案诸元的值,对目标进行打击.’%Combining analytical prediction and optimization of parameters, a rapid method for basic firing data of flight program of the ballistic missile launched on mobile platform is studied. First, the analytical expressions between the parameters about flight program and attack information are obtained by using polynomial function approximation, by which the initial value of the firing data can be calculated. Second, considering the parameters of flight program as variables and the least square of the placements aberration as the performance index, the Levenberg-Marquardt (L-M) Method is used to obtain the optimal values. Finally, as an example, the proposed method is provided to attacking targets with the LMG-30G. The simulation results show that, because of the less computational effort, the proposed method is suitable for the rapid design of the Big Wide Intratheater Mobility for the missile. When the precision of the placement is not highly demanded, the solution of analytical expressions can be used directly as the value of flight parameters to attack the target.

  14. New Changes of Fire Tactics in Air Defense Forces Group Missile for Equipment Authorization%编配某型导弹的防空兵群火力运用新变化

    Institute of Scientific and Technical Information of China (English)

    王仁芳; 王巨海; 韩校粉

    2013-01-01

    某新型地空导弹列装部队,给部队作战能力提升带来革命性变化,结合新型导弹的作战优势,阐述了防空兵群火力运用新变化,进一步提出了提高防空兵群火力运用效能的对策。%íí Ground-to-air Missile incorporated in army, this brings large affects for the advancing of operational capability in army. Based the campaign superiority of new Missile,it expatiates the new changes of fire tactics of Air Defense Forces Group and brought forward more countermeasures to advance the efficiency of fire tactics of Air Defense Forces Group.

  15. 基于多Agent建模的弹道导弹多特征综合识别框架%Multi-feature Fusion Identification Framework for Ballistic Missile Based on Multi-agent Modeling

    Institute of Scientific and Technical Information of China (English)

    田康生; 李鸿飞; 金宏斌; 吴长飞

    2016-01-01

    It is difficult for radar to implement ballistic missile identification successfully, and it needs to integrate the capabilities of intelligence, self-adaption and cooperation for the identification system. On the basis of traditional identification methods, a multi-feature fusion identification framework based on multi-agent modeling is presented. The reference rule base and internal state base of the agents are established. The process procedure and interactive relationship of agents are given. The simulation based on Swarm platform shows that the multi-feature fusion identification framework can implement fusion identification effectively with correct recognition result.%由于弹道导弹目标特征具有积累时间各异、分类方法繁多、存在干扰等难点,需要系统具备智能、自适应和协作的能力来完成目标的综合识别。在传统综合识别的基础上,提出了一种基于多Agent建模的弹道导弹多特征综合识别框架,构建了Agent的推理规则库和内部状态库,描述了Agent的处理流程与交互关系。基于Swarm平台仿真验证表明,该框架能有效进行多特征综合识别,给出正确的识别结果。

  16. Technical development and application of primary battery for air defense missile%防空导弹弹上电池技术的发展及应用

    Institute of Scientific and Technical Information of China (English)

    蔡绍伟

    2012-01-01

    防空导弹普遍采用弹上电池作为弹上主电源,经历了铅酸电池、锌银电池到热电池三个发展阶段.介绍了锌银电池,钙-铬酸钙体系、锂及锂合金-二硫化铁体系热电池技术的发展、性能特点及国内外发展现状.论述了锌银储备电池及热电池的组成、工作原理和技术优势.指出了防空导弹弹上电池技术的发展方向.%The technical development,performance and developing status of Zn/AgO battery both in China and abroad,calcium/calcium chromate system,and lithium (lithium alloy)/iron disultide system thermal batteries were introduced.The structure,principle and technical advantages of Zn/AgO battery and thermal battery were discussed.Finally,some development directions of the primary battery for air defense missile were also forecasted.

  17. 印度导弹武器装备体系发展与前景分析%Analysis of Indian Missile Weapon System Development

    Institute of Scientific and Technical Information of China (English)

    张莹

    2012-01-01

    随着国际安全环境的重大变化,印度加紧了其军事战略的调整和军队建设的步伐,大力发展导弹武器体系建设,对周边国家和地区形成了安全威胁.在分析印度军事战略的基础上,重点阐述印度弹道导弹、巡航导弹、防空导弹和导弹防御系统等武器装备体系的建设情况,并分析了其发展趋势和未来前景.%With the tremendous changes of the international security environment, India promotes the military strategy adjustment and the military construction, and pays great attention to the development of missile weapon system, threatening to the security of neighboring countries and regions. Beginning with the Indian military strategy, this paper describes the Indian weapon system construction in depth, such as the ballistic missile, cruise missile, air defense system and ballistic missile defense system .ete. Finally future development trend and prospect are analyzed.

  18. The Research on the Influence Relationships of Combat Capabilities of Air-defense Missile System Based on Probability Influence Diagram%概率影响图的防空导弹作战能力影响分析

    Institute of Scientific and Technical Information of China (English)

    张思滨; 黄金才; 朱承; 乔士东

    2012-01-01

    Aiming to the problem of being hard to evaluate quantitatively about the influence relationships of each combat capability of Air-Defense Missile System, the paper presents a method which analyzes the problem based on probability influence diagram. As the precondition, the Air-Defense Missile combat flow should be analyzed and the influence relationships of each combat activity should be ascertained. First of all, the paper estimates the edged and conditioned probabilities of each combat capability based on the influence relationships of combat activities. Secondly, it builds the probability influence diagram of Air-Defense Missile System based on target oriented method. In the end, it estimates the influence relationships of each combat capability quantitatively based on the consistency transform, which gets the key capability index and analyzes probability changing degree of influence relationships dynamically. We analyze PAC-3 Tactics Air-defense Missile System as a example, the result shows that the method of probability influence diagram is feasible and valid for the research on the influence relationships of combat capabilities of Air-Defense Missile System.%针对防空导弹系统各作战能力间影响关系难以量化评估的问题,提出利用概率影响图进行分析的方法.在分析防空导弹作战流程、确定各作战活动影响关系的前提下,该方法首先由作战活动影响关系估计各作战能力结点的边缘概率和条件概率;其次利用目标定向法建立防空导弹作战能力概率影响图;最后对概率影响图进行一致性变换,定量评估各作战能力间的影响关系,寻找重要能力指标,并动态分析影响关系的概率变化.以战术级爱国者防空导弹系统PAC-3为例借助该方法进行分析.结果证明,利用概率影响图分析防空导弹作战能力影响关系是可行和有效的.

  19. Guidance Law Based on Differential Geometry for Endo-atmosphere Tactical Ballistic Missile Interceptor%基于微分几何的拦截弹制导律研究∗

    Institute of Scientific and Technical Information of China (English)

    武唯强; 陈康; 符文星; 闫杰; 陈凯

    2015-01-01

    针对战术导弹的拦截问题,根据质点微分几何运动学在弧长系下及在时域内的关系,将弧长系下的微分几何制导律应用到实际的TBM拦截过程中,得到了空间中时域内的微分几何制导律以及相应的过载指令。根据拦截过程中目标的不同机动方式,采用微分几何制导与比例导引进行了仿真对比与分析,得到了两种导引律下的脱靶量与拦截时间。仿真结果表明,微分几何制导律能够在拦截过程中降低视线角速度并使其趋于稳定,在拦截开始其过载需求较大并逐渐降低至接近0,脱靶量及拦截时间都小于比例导引律,采用微分几何制导律能够在更短时的时间内进行精确拦截。%In this paper, the endo⁃atmosphere tactical ballistic missile interceptor is studied, especially on the terminal guidance law. According to the relationship between arc system and time domain, differential geometry guidance law will be applied to the process of TBM interception. Differential geometric guidance law and the relative overload command in the time domain of 3D space is derived. When it is compared with the classic proportion navigation law in the simulation toward a high speed maneuvering target, the designed differential geometry guidance law demonstrates its superiority by an obviously lower miss distance and lower line of sight rate.

  20. Laser beam riding artillery missiles guidance device is designed

    Science.gov (United States)

    Yan, Mingliang; Huo, Zhicheng; Chen, Wei

    2014-09-01

    Laser driving gun missile guidance type beam of laser information field formed by any link failure or reduced stability will directly lead to ballistic or miss out of control, and based on this, this paper designed the driving beam of laser guided missile guidance beam type forming device modulation and zoom mechanism, in order to make the missile can recognize its position in the laser beam, laser beam gun missile, by means of spatial encoding of the laser beam laser beam into information after forming device, a surface to achieve the purpose of precision guidance.

  1. 防空导弹武控设备实现CBM方法的探讨%Research on the Condition Based Maintenance for Weapon Control Equipment of Air-defense Missile

    Institute of Scientific and Technical Information of China (English)

    曲宏宇; 向哲

    2012-01-01

    针对解决防空导弹武控设备目前维修方式中的诸多问题,基于状态的维修(CBM)方式是有效解决途径之一。分析了对防空导弹武控设备进行CBM时的状态监测、失效模型建立、故障预测和维修决策等关键技术问题,探讨了防空导弹武控设备实现CBM的技术对策。结果表明,CBM具有诸多优点,它的实践应用必将引发武控设备维修技术的根本变革,促进高新技术在防空导弹武控设备维修领域的应用。%The condition based maintenance(CBM) is one of effective maintenance methods for weapon control equipment of air-defense missile.The key techniques is analyzed about inspecting the condition,establishing invalidation modal,forecasting malfunction,maintenance decision-making of CBM that is used for weapon control equipment of air-defense missile,the technique countermeasure of carrying CBM is introduced.The results show CBM is effective,which will result in radical change in maintenance technique of weapon control equipment,and promote using of new techniques in maintenance for weapon control equipment of air-defense missile.

  2. Toward a defense-dominated world

    Energy Technology Data Exchange (ETDEWEB)

    Wood, L.

    1993-08-01

    Maintaining the large-scale peace in a defense-dominated world necessarily will require not only passive but also active defenses against large-scale aggression that are technically feasible, practical and easy to employ -- and robust against perversion into support of aggression. Such peace maintenance tool-sets will feature means for effectively rebuking aggression as well as providing timely and very widely available seaming of aggression underway anywhere. This report discusses the technology base which currently exists to provide world-wide, high-quality imagery at moderate (5--10 meter) spatial resolution or imagery of 1% of the Earth`s land surface at high ({le} 1 meter) resolution no less frequently than daily, at a total cost of the order of $1 B, with operational capability in the later `90s. Such systems could provide timely warning of aggressive actions anywhere. Similarly, space-based means of defeating aggression conducted with even quite short-range ballistic missiles anywhere in the world could be brought into existence by the end of the `90s for a total cost of about $10 B, and small high-altitude, long flight-duration robotic aircraft carrying high-performance sensors and interceptor missilery could provide both seaming and active defenses against attacks conducted with very short range ballistic missiles, as well as attacks launched with air-breathing threats such as bombers and cruise missiles, for a cost per defended area of the order of $10/km{sup 2}. It appears that all of the associated sensors can find apt dual-use as high-performance systems for monitoring physical aspects of the human environment.

  3. 防空导弹武器系统通用火控软件设计与实现%General Design and Accomplishment of Firepower Control Software in Air Defense Missile Weapon System

    Institute of Scientific and Technical Information of China (English)

    陈华

    2011-01-01

    针对不同防空导弹武器系统的火控软件之间不能互用的现状,分析了火控系统各主要功能模块之间的接口关系,提出了火控软件通用化设计的思路,并用C++实现了该设计.火控软件的通用化设计值碍将来防空导弹能武器系统火控软件的标准化设计和编程借鉴.%s :Contrasting the status of no interoperability in firepower control softwares among different aerial defense missile weapon system, the interface relation of functional module in firepower control system is analyzed.And the idea of general design of firepower control software is put forward.Furthermore, the idea is realized by using C++ programming.The general design of firepower control software is worth used for reference in the standard design and programming of future aerial defense missile weapon system.

  4. Probabilistic Analysis of Anti-ship Missile Defence Effectiveness

    Directory of Open Access Journals (Sweden)

    Debasis Dutta

    2014-03-01

    Full Text Available Effective missile defence systems are primary requirement for naval ships to counter lethal anti-ship cruise missile attacks in today’s naval warfare scenario. Anti-ship ballistic missiles would further add worry to ship missile defence. The paper discusses a probabilistic analysis of missile defence system effectiveness by considering a simple scenario of a single ship defence with multiple interceptors against a single non-maneuvering missile attack. The ship’s interceptor hard kill lethality is taken as the measures of effectiveness in the analysis. The paper discusses effect of different firing policies, multi-sensor and layered defence to achieve maximum ship survivability.Defence Science Journal, 2014, 64(2, pp. 123-129. DOI: http://dx.doi.org/10.14429/dsj.64.3532

  5. First Soviet Sea-Launched Ballistic Rockets

    Directory of Open Access Journals (Sweden)

    Yuri F. Katorin

    2013-03-01

    Full Text Available In the article it is told about the creation of the first generation of Soviet ballistic missiles for the armament of submarines. The basic stages of their development, tests and adoption for the armament are described. Are cited the data about the people, is most which actively participated in these processes.

  6. Heat-Transfer and Pressure Measurements from a Flight Test of the Third 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.86 and Reynolds Number per Foot of 23.5 x 10(exp 6) and a Comparison with Heat Transfer

    Science.gov (United States)

    Graham, John B., Jr.

    1958-01-01

    Heat-transfer and pressure measurements were obtained from a flight test of a 1/18-scale model of the Titan intercontinental ballistic missile up to a Mach number of 3.86 and Reynolds number per foot of 23.5 x 10(exp 6) and are compared with the data of two previously tested 1/18-scale models. Boundary-layer transition was observed on the nose of the model. Van Driest's theory predicted heat-transfer coefficients reasonably well for the fully laminar flow but predictions made by Van Driest's theory for turbulent flow were considerably higher than the measurements when the skin was being heated. Comparison with the flight test of two similar models shows fair repeatability of the measurements for fully laminar or turbulent flow.

  7. 基于微分对策的拦截末段突防导弹机动突防制导律研究%Study on Maneuver Penetration Guidance Law of Ballistic Missile Based on Differential Games in the Terminal of Interception

    Institute of Scientific and Technical Information of China (English)

    张士熊; 刘新学; 李斌; 孟少飞

    2015-01-01

    For improving the penetration performance of ballistic missile in the terminal of the interception course, this paper analyzes the maneuver penetration guidance law of ballistic missile based on three-dimensional differential games theory. Based on the line of sight angle rate, a moving model about the interception-penetration is set up. And then an optimal guidance law in the terminal of interception is derived about the two parties. Finally, a simulation platform is set up, and simulation is repeated based on different parameter groups. The result of simulation shows that, the penetration guidance law raised in this paper can make a miss distance up to 12 meters with an obvious penetration effect.%为提高弹道导弹在拦截末段机动突防性能,基于微分对策理论对三维空间中的机动突防制导律进行研究。从视线倾角和视线偏角的变化率模型出发建立拦截-突防双方的运动模型;推导了双方在拦截末段的最优制导律;在Simulink下搭建仿真平台,并选取不同参数组合进行多次仿真。仿真结果表明,本文提出的突防制导律可使脱靶量达到12m,突防效果明显。

  8. Study on Maneuver Penetration Guidance Law of Ballistic Missile Based on Differential Games in the Terminal of Interception%基于微分对策的拦截末段突防导弹机动突防制导律研究

    Institute of Scientific and Technical Information of China (English)

    张士熊; 刘新学; 李斌; 孟少飞

    2015-01-01

    为提高弹道导弹在拦截末段机动突防性能,基于微分对策理论对三维空间中的机动突防制导律进行研究。从视线倾角和视线偏角的变化率模型出发建立拦截-突防双方的运动模型;推导了双方在拦截末段的最优制导律;在Simulink下搭建仿真平台,并选取不同参数组合进行多次仿真。仿真结果表明,本文提出的突防制导律可使脱靶量达到12m,突防效果明显。%For improving the penetration performance of ballistic missile in the terminal of the interception course, this paper analyzes the maneuver penetration guidance law of ballistic missile based on three-dimensional differential games theory. Based on the line of sight angle rate, a moving model about the interception-penetration is set up. And then an optimal guidance law in the terminal of interception is derived about the two parties. Finally, a simulation platform is set up, and simulation is repeated based on different parameter groups. The result of simulation shows that, the penetration guidance law raised in this paper can make a miss distance up to 12 meters with an obvious penetration effect.

  9. 美军2020联合一体化防空反导构想浅析%The USA vision for 2020 joint integrated air and missile defense

    Institute of Scientific and Technical Information of China (English)

    阙渭焰

    2016-01-01

    The USA vision for 2020 joint integrated air and missile defense (IAMD) is analyzed .The IAMD related strategic and threat environments are unscrambled ,around the core of the intent for IAMD vision .Six key imperatives for joint IAMD vision are encapsulated .The whole status of IAMD is clearly described .%对美军2020联合一体化防空反导(IAMD)构想进行了分析。围绕这个构想的核心思想,解读了美军联合IAMD力量体系所面临的全球战略环境和战区环境;突出构想六个方面的要点,介绍了美军联合IA M D力量体系未来发展的全貌。

  10. Missile Design Toolbox

    OpenAIRE

    Ekker, David A.

    1994-01-01

    Missile Design (MSLDSN) is a toolbox created to be used with The MathWorks' MATLAB® interactive computing environment, version 4.2. MSLDSN provides the missile deSigner with a number of tools to aid in establishing and evaluating missile parameters during the conceptual phase of design. MSLDSN aids the designer in establishing an initial configuration which is then refined using the various missile programs (e.g .• Missile Datcom). MSLDSN is limited to designing solidpropellant- ...

  11. A robust approach to the missile defence location problem

    NARCIS (Netherlands)

    Bloemen, A.A.F.; Evers, L.; Barros, A.I.; Monsuur, H.; Wagelmans, A.P.M.

    2011-01-01

    This paper proposes a model for determining a robust defence strategy against ballistic missile threat. Our approach takes into account a variety of possible future scenarios and different forms of robustness criteria, including the well-known absolute robustness criterion. We consider two problem v

  12. Detecting Simulation of Trajectory of Tactical Ballistic Missile Using Space-Based Early Warning Satellite%天基预警卫星弹道预报能力仿真分析

    Institute of Scientific and Technical Information of China (English)

    曾番; 李晓军; 李国宏; 冯卉

    2013-01-01

    Space-based early warning satellites can forecast the errors of ballistic position and velocity which is the important component of guidance information and directly influence search performance of long-range early warning radar and tracking and guiding radar.According to give information about the Line-of-Sight (LOS) angular errors of the satellites and their ballistic target empirical data,ballistic prediction error estimation modeland compute prediction error bands is designed.The simulations show that horizontal and vertical plane prediction error bands of viewing satellites can be obtained by analyzing observation errors covariance for ideal trajectory target.%天基预警卫星对导弹位置和速度的预测误差是引导信息中的重要组成部分,直接影响到远程预警雷达和跟踪制导雷达的搜索性能.根据天基预警卫星视线角误差和导弹目标经验数据,设计导弹预报误差估计模型,计算预报误差带半径.仿真结果表明:通过对理想弹道目标进行观测误差协方差分析,可以获得预警卫星观测的水平及垂直平面预测误差带.

  13. Research on Efficiency Evaluation Model That Air Defense Missile and Artillery Resist Multiple Targets in Coordination%舰空导弹与火炮武器协同抗击多目标的效能评估

    Institute of Scientific and Technical Information of China (English)

    由大德; 徐德民; 张发强

    2011-01-01

    In order to make the air defense and artillery weapon are used significantly, and improve the operational efficiency that resisting the multiple targets, on base analyzing the emitter region of the missile and artillery weapon, by means of studying the shooting times of multiple air defense weapon shooting tunnels and shooting mode and shooting times of the artillery weapon, it established the optimal model efficiency evaluation,at last it defined the optimal firepower distribution schemes by means of an example based on the model, it verified the use of the model.%为使水面舰艇防空导弹与火炮武器有效协同使用,提高抗击空袭多目标的作战效能,在分析防空导弹和近防炮武器发射区的基础上,通过研究防空导弹多个射击通道的射击次数、火炮武器的射击方式和射击次数等,建立了协同抗击多目标的效能评估模型,并运用该模型对确定最优火力分配方案的使用方法进行了举例分析,验证了模型的可用性.

  14. Terminal Ballistics

    CERN Document Server

    Rosenberg, Zvi

    2012-01-01

    This book covers the important issues of terminal ballistics in a comprehensive way combining experimental data, numerical simulations and analytical modeling. The first chapter reviews the experimental equipment which are used for ballistic tests and the diagnostics for material characterization under impulsive loading conditions. The second chapter covers essential features of the codes which are used for terminal ballistics such as the Euler vs. Lagrange schemes and meshing techniques, as well as the most popular material models. The third chapter, devoted to the penetration mechanics of rigid penetrators, brings the update of modeling in this field. The fourth chapter deals with plate perforation and the fifth chapter deals with the penetration mechanics of shaped charge jets and eroding long rods. The last two chapters discuss several techniques for the disruption and defeating of the main threats in armor design. Throughout the book the authors demonstrate the advantages of numerical simulations in unde...

  15. Impacts of Deflection Nose on Ballistic Trajectory Control Law

    Directory of Open Access Journals (Sweden)

    Bo Zhang

    2014-01-01

    Full Text Available The deflection of projectile nose is aimed at changing the motion of the projectile in flight with the theory of motion control and changing the exterior ballistics so as to change its range and increase its accuracy. The law of external ballistics with the deflectable nose is considered as the basis of the design of a flight control system and an important part in the process of projectile development. Based on the existing rigid external ballistic model, this paper establishes an external ballistic calculation model for deflectable nose projectile and further establishes the solving programs accordingly. Different angle of attack, velocity, coefficients of lift, resistance, and moment under the deflection can be obtained in this paper based on the previous experiments and emulation researches. In the end, the author pointed out the laws on the impaction of external ballistic trajectory by the deflection of nose of the missile.

  16. Converting the Minuteman missile into a small satellite launch system

    Science.gov (United States)

    Alexander, Bill; Gonzalez, Rodolfo; Humble, Greg; Mackay, Gordon; Mchaty, Rod; Pham, VU

    1993-01-01

    Due to the Strategic Arms Reduction Talks (START) treaty between the United States and Ex-Soviet Union, 450 Minuteman 2 (MM 2) missiles were recently taken out of service. Minotaur Designs Incorporated (MDI) intends to convert the MM 2 ballistic missile from a nuclear warhead carrier into a small satellite launcher. MDI will perform this conversion by acquiring the Minuteman stages, purchasing currently available control wafers, and designing a new shroud and interfaces for the satellite. MDI is also responsible for properly integrating all systems.

  17. Six-Degree-of-Freedom Digital Simulations for Missile Guidance and Control

    Directory of Open Access Journals (Sweden)

    Yongjie Xu

    2015-01-01

    Full Text Available Six-degree-of-freedom ballistic trajectory model can be used to verify design indicators, performance parameters, and correctness so they have been put forward in the missile argumentation and design process. Mathematical simulation is the basis of late semiphysical simulation and field firing testing, and it can greatly reduce the field shooting test time, which shortens the missile test cycle and so reduces costs.

  18. Research on Interception Coalition Formation in Networked Air Defense Missile Systems%网络化防空导弹体系拦截联盟形成问题

    Institute of Scientific and Technical Information of China (English)

    唐苏妍; 朱一凡; 葛伟; 雷永林; 李群

    2012-01-01

    Interception Coalition Formation (ICF) is one of the cutting-edge problems in Networked Air Defense Missile Systems (NADMS) research, aiming to allocate the most suitable weapons and guidance radars to the targets, so as to maximize the effectiveness of NADMS. With analysis of the distributed flexible network architecture of NADMS, we specifically explored the hypostasis of ICF and defined five new cooperative NADMS engagement strategies. The problem of ICF is formalized separately in three aspects of operations research and integer programming, combinatorial optimization, and economics gaming. Both centralized and distributed ICF methods are discussed in detail as well under these formalisms.%拦截联盟形成是网络化防空导弹体系(NADMS)中的新问题,旨在确定目标、火力节点以及制导节点三者之间的最优匹配关系,使得NADMS整体作战效能最大.结合NADMS的分布式无中心节点体系结构,剖析了拦截联盟形成问题的本质,形式化定义了体系中出现的新型一体化作战能力;分别从运筹学与整数规划、组合优化以及经济学博弈问题角度对拦截联盟形成问题进行形式化描述,并深入探讨了集中式和分布式的拦截联盟形成方法.

  19. UV missile plume signatures

    NARCIS (Netherlands)

    Neele, F.P.; Schleijpen, H.M.A.

    2002-01-01

    As a result of the deployment of UV missile warning systems, recent years have seen an increasing interest in threat assessment in the UV band. Unfortunately, due to the different nature of the physical processes that are needed to describe a missile signature in the UV, available codes for the IR c

  20. 基于星光测量天基传感器实时定标在弹道目标跟踪应用%Space-based Sensor Online Calibration Based on Celestial Observations for Tracking Ballistic Missile Target

    Institute of Scientific and Technical Information of China (English)

    俞建国; 刘梅; 包玖红; 姚璐

    2013-01-01

    The systemic bias of space-based sensor hinders accurate threat identification and target location of coming targets. The correction of this systematic bias has unique difficulties including unable to in-situ commissioning and systemic bias periodically change as the satellite undergoes a cyclical heating and cooling due to its orbit. Combining the satellite altitude determination system, this paper firstly obtains the star vector measurement from electro-optical sensor and monitors the deviation of these measurements from expected value in navigation star table. Then, on the basis of systemic bias, this paper derives bias model and design the Bias Corrected Shift Rayleigh Filter (BCSRF). Simulation results show that the proposed filter can achieve in-situ calibration, and yields significant improvements in tracking ballistic targets compared with classical intersection and Unscented Kalman Filter (UKF) methods.%  天基传感器的系统偏差妨碍了对来袭目标的准确识别与定位,而该系统偏差修正存在着其特有的难点:无法现场调试及系统偏差随着轨道变化导致卫星温度冷热交替呈周期性变化。该文结合卫星姿态确定系统,首先利用光电传感器获得恒星的星光矢量测量值并时刻监测星光矢量与导航星表中预期值的偏差;其次在获得系统偏差测量值基础上推导了偏差模型,设计了基于BCSRF(Bias Corrected Shift Rayleigh Filter)自由段弹道目标跟踪滤波器。仿真实验表明该滤波器能够实现在线定标功能,同等条件下与传统的交叉定位和UKF(Unscented Kalman Filter)滤波方法相比,有效提高了自由段弹道目标的跟踪精度。

  1. Terminal ballistics

    CERN Document Server

    Rosenberg, Zvi

    2016-01-01

    This book comprehensively discusses essential aspects of terminal ballistics, combining experimental data, numerical simulations and analytical modeling. Employing a unique approach to numerical simulations as a measure of sensitivity for the major physical parameters, the new edition also includes the following features: new figures to better illustrate the problems discussed; improved explanations for the equation of state of a solid and for the cavity expansion process; new data concerning the Kolsky bar test; and a discussion of analytical modeling for the hole diameter in a thin metallic plate impacted by a shaped charge jet. The section on thick concrete targets penetrated by rigid projectiles has now been expanded to include the latest findings, and two new sections have been added: one on a novel approach to the perforation of thin concrete slabs, and one on testing the failure of thin metallic plates using a hydrodynamic ram.

  2. MISSILES AND AIRCRAFT - PART 4

    Directory of Open Access Journals (Sweden)

    C. Meyer

    2012-02-01

    Full Text Available This Article, the last of four concerning the role of air power in the Yom Kippur War, analysis the following: Missile effectiveness - (surface-to-air missiles, air-to-surface missiles, surface-to-surface missiles. Aerial combat and pilot training. Electronic warfare, Precision Guided Munitions and Remotely Piloted Vehicles. The use of satellites for real time intelligence.

  3. Characteristics of tornado generated missiles

    International Nuclear Information System (INIS)

    The development of techniques designed to calculate tornado missile velocities is traced. It is shown that there is a need for a consistent method for obtaining missile velocities for a variety of tornado parameters. A consistent method for determination of trajectories and velocities of missiles generated by a tornado is described. The effects of plant layout upon missile impact velocity at a given building are discussed from the point of view of determining the necessary missile barrier characteristics. 19 references

  4. Ballistic trajectories

    Science.gov (United States)

    Bender, D. F.

    1978-01-01

    The only ballistic trajectory mode feasible for a close solar probe or for an orbit inclined approximately 90 degrees to the ecliptic is the Jupiter gravity assisted mode. A comparison of the trajectories of the Solar Polar and the Solar Probe Mission for 1983 launches is shown. The geometry of the solar encounter phase is practically the same for the 4.3 year orbit achieved by a Jupiter gravity assist and for a one year orbit. Data describing the geometry of an orbit with perihelion at 4 solar radii and aphelion at Jupiter are listed. The range of apparent directions of the solar wind if it is flowing radially outward from the Sun with a speed of either 150 or 300 km/sec is shown. The minimum sun-earth-probe angle during the solar encounter as a function of the earth-node angle and the orbital inclination is also shown. If the inclination is 60 degrees or more, the minimum SEP angle is not greatly different from the 90 degree value.

  5. Centralized interception coalition formation method in networked air defense missile systems%网络化防空导弹体系集中式拦截联盟形成方法

    Institute of Scientific and Technical Information of China (English)

    唐苏妍; 朱一凡; 葛伟; 李群

    2011-01-01

    Centralized interception coalition, which focuses on the method to allocate the targets, shooters and guidance sensors in order to maximize the effectiveness of the system, is one of the new problems in Networked Air Defense Missile Systems. According to the operational context, a constrained optirnization model was proposed for the problem and the particle swarm optimization algorithm was chosen to solve the model. To solve the local optimization problem of the algorithm, the creative thinking was introduced into particles from the cognitive psychology aspects. It is considered that creative thinking can improve the cognitive capability of particles to prevent the premature convergence problem. Based on the classical four-phase model in creative thinking process, a framework of creative thinking based particle swarm optimization algorithm was provided by adapting the evolution model. According to discrete characteristics of the problem, a discrete strategy was designed by setting the coding rules and the operation rules for particles' velocity and position. Experimental results show that the proposed algorithm has priority in solution quality and convergence rate.%集中式拦截联盟(CIC)形成是网络化防空导弹体系(NADMS)中的新问题,旨在确定目标、火力节点以及制导节点三者之间的最优匹配关系,以使得体系整体作战效能最大.根据问题背景,建立了CIC的约束优化问题模型,并选择收敛速度较快的粒子群优化(PSO)算法对模型进行求解.针对PSO的局部收敛问题,从认知心理学角度将人类特有的创造性思维(CT)引入粒子速度更新公式中,通过提升单个粒子的搜索能力来提高整个群体的寻优质量.基于CT过程经典的四阶段模型构建了算法框架,改进了PSO的速度更新公式.根据CIC问题特点,制定了编码策略及相关变量的离散化运算规则.实验结果证明了算法在CIC问题求解质量和收敛速度方面的优越性.

  6. Nanotechnology for missiles

    Science.gov (United States)

    Ruffin, Paul B.

    2004-07-01

    Nanotechnology development is progressing very rapidly. Several billions of dollars have been invested in nanoscience research since 2000. Pioneering nanotechnology research efforts have been primarily conducted at research institutions and centers. This paper identifies developments in nanoscience and technology that could provide significant advances in missile systems applications. Nanotechnology offers opportunities in the areas of advanced materials for coatings, including thin-film optical coatings, light-weight, strong armor and missile structural components, embedded computing, and "smart" structures; nano-particles for explosives, warheads, turbine engine systems, and propellants to enhance missile propulsion; nano-sensors for autonomous chemical detection; and nano-tube arrays for fuel storage and power generation. The Aviation and Missile Research, Development, and Engineering Center (AMRDEC) is actively collaborating with academia, industry, and other Government agencies to accelerate the development and transition of nanotechnology to favorably impact Army Transformation. Currently, we are identifying near-term applications and quantifying requirements for nanotechnology use in Army missile systems, as well as monitoring and screening research and developmental efforts in the industrial community for military applications. Combining MicroElectroMechanical Systems (MEMS) and nanotechnology is the next step toward providing technical solutions for the Army"s transformation. Several research and development projects that are currently underway at AMRDEC in this technology area are discussed. A top-level roadmap of MEMS/nanotechnology development projects for aviation and missile applications is presented at the end.

  7. Advanced missile technology. A review of technology improvement areas for cruise missiles. [including missile design, missile configurations, and aerodynamic characteristics

    Science.gov (United States)

    Cronvich, L. L.; Liepman, H. P.

    1979-01-01

    Technology assessments in the areas of aerodynamics, propulsion, and structures and materials for cruise missile systems are discussed. The cruise missiles considered cover the full speed, altitude, and target range. The penetrativity, range, and maneuverability of the cruise missiles are examined and evaluated for performance improvements.

  8. The proliferation of massive destruction weapons and ballistic missiles

    International Nuclear Information System (INIS)

    The author studies the actual situation of nuclear deterrence policies, the possibilities of use chemical weapons as massive destructions weapons for non nuclear governments. The situation of non proliferation of nuclear weapons took a new interest with the disintegration of the communism block, but it seems that only few nuclear matter disappeared towards proliferating countries. The denuclearization of Bielorussia, Ukraine and Kazakhstan makes progress with the START I treaty; China has signed the Non proliferation treaty in 1992, it conducts an export policy in matter of equipment and know-how, towards Iran, Pakistan, North Korea, Saudi Arabia and Syria. In a future of ten years, countries such, Iran, North Korea could catch up with Israel, India and Pakistan among non declared nuclear countries. For chemical weapon, Libya, Iran and Syria could catch up with Iraq. (N.C.)

  9. Military and diplomatic roles and options for managing and responding to the proliferation of ballistic missiles and weapons of mass destruction. Final report: Program on Stability and the Offense/Defense Relationship

    Energy Technology Data Exchange (ETDEWEB)

    Hallenbeck, R.A.; Gill, J.M.; Murray, B.L.

    1993-05-26

    The March seminar, ``Military and Diplomatic Roles and Options`` for managing and responding to proliferation, featured three presentations: the military and diplomatic implications of preemptive force as a counterproliferation option; an in-depth assessment of the threat posed by biological weapons; and, a new proposed US counterproliferation policy.

  10. Missile injuries in head — neck and maxillo-facial region — an experience in eastern nepal

    OpenAIRE

    Wakode, P. T.; Ghimire, Anand; Acharya, Roshan

    2008-01-01

    Ballistic injuries to head-neck and maxillofacial region is quite common problem nowadays. Most of the time the injuries seem to be dreadful but the mechanism of the injuries caused by ballistics and the anatomical conditions of maxillofacial and head-neck region mitigate the severity of the injuries. Proper primary management followed by reconstruction and management of associated injuries decreases the mortality and morbidity of missile injuries in head-neck and maxillofacial region. Eleven...

  11. 便携式防空导弹发射区优化仿真研究∗%Research on Simulation of Portable Air Defense Missile Launch Envelops Optimization

    Institute of Scientific and Technical Information of China (English)

    吴豫杰; 郑国民; 刘虎

    2015-01-01

    发射区是一个空间区域,当目标处于该空域内不同子域时发射导弹,导弹对目标的杀伤概率不尽相同。为寻求发射区内最佳发射时机,提高导弹的作战效能,对发射区进行等步长离散,计算特征点脱靶量,选取最优发射区域。基于便携式防空导弹仿真平台,以某型便携式防空导弹为算例进行分析,得出发射区内不同子域脱靶量分布的一般规律,为射手和指挥员确定导弹发射时机提供依据。%Launch area is a large space, when target is in different subdomains;the kill probability of missile is not the same. For seeking the best fire time and improving combat effectiveness, the launch area was discrete, the value of miss distance at characteristic point was calculated and the optimal launch area was selected. The method of missile envelops optimization was put forward. Based on simulation platform of portable surface-to-air missile, the simulation result that a certain type of portable surface-to-air missile shooting a certain type of target drone was analyzed, the distribution law of the miss distance in the launch area was obtained, and a reference that how to choose the fire opportunity for shooter and commander was provided.

  12. Tornado missile impact study

    International Nuclear Information System (INIS)

    UCRL-15910 specifies wind and tornado missiles for moderate- and high-hazard DOE facilities. Wall-barrier specimens have been tested at the Tornado Missile Impact Facility at Texas Tech University. The facility has an air-activated tornado missile cannon capable of firing 2x4 timber planks weighing 12 lb at speeds up to 150 mph and 3-in-diameter steel pipes weighing 75 lb at speeds to 7 5 mph. Wall barriers tested to date include reinforced concrete walls from 4-in. to 10-in. thick; 8-in. and 12-in. walls of reinforced concrete masonry units (CMU); two other masonry wall configurations consisting of an 8-in. CMU with a 4-in. clay-brick veneer and a 10-in. composite wall with two wythes of 4-in. clay brick. The impact test series is designed to determine the impact speed that will produce backface spall of each wall barrier. A set of 15 wall sections has been constructed and tested at this time. Preliminary finding suggest that all cells of CMU walls must be grouted to prevent missile penetration. Walls recommended in the workshop on UCRL-15910 provide acceptable protection if cracking can be accepted

  13. 77 FR 40693 - Bureau of Political-Military Affairs: Directorate of Defense Trade Controls; Notifications to the...

    Science.gov (United States)

    2012-07-10

    ... Active Layered Theater Ballistic Missile Defence Systems Engineering and Integration Contract. The United... Globemaster III Transport Aircraft, Wing Trailing Edge Panels and Flap Hinge Fairings for end-use by a...

  14. CMC occasional papers : a missile stability regime for South Asia.

    Energy Technology Data Exchange (ETDEWEB)

    Khan, Feroz Hassan (Pakistan Army, Islamabad, Pakistan); Vannoni, Michael Geoffrey; Rajen, Gaurav (Gaia Research Consulting, Albuquerque, NM)

    2004-06-01

    India and Pakistan have created sizeable ballistic missile forces and are continuing to develop and enlarge them. These forces can be both stabilizing (e.g., providing a survivable force for deterrence) and destabilizing (e.g., creating strategic asymmetries). Missile forces will be a factor in bilateral relations for the foreseeable future, so restraint is necessary to curtail their destabilizing effects. Such restraint, however, must develop within an atmosphere of low trust. This report presents a set of political and operational options, both unilateral and bilateral, that decreases tensions, helps rebuild the bilateral relationship, and prepares the ground for future steps in structural arms control. Significant steps, which build on precedents and do not require extensive cooperation, are possible despite strained relations. The approach is made up of three distinct phases: (1) tension reduction measures, (2) confidence building measures, and (3) arms control agreements. The goal of the first phase is to initiate unilateral steps that are substantive and decrease tensions, establish missiles as a security topic for bilateral discussion, and set precedents for limited bilateral cooperation. The second phase would build confidence by expanding current bilateral security agreements, formalizing bilateral understandings, and beginning discussion of monitoring procedures. The third phase could include bilateral agreements limiting some characteristics of national missile forces including the cooperative incorporation of monitoring and verification.

  15. Detection Performance Assessment of Ground-Based Phased Array Radar for Ballistic Targets%地基相控阵雷达对弹道目标的探测性能评估

    Institute of Scientific and Technical Information of China (English)

    李星星; 姚汉英; 孙文峰

    2014-01-01

    为解决地基相控阵雷达对弹道目标探测的最优部署问题,建立弹道中段目标轨道运动和进动模型,提出弹道中段多部地基相控阵雷达的弹道目标探测概率模型,以及平均检测概率、稳定跟踪时间和资源冗余时间3种组合的雷达探测性能评估指标。依据弹道目标RCS及探测距离随观测时间的变化情况,通过仿真实验对多种部署方式下地基雷达对弹道目标探测性能评估指标的分析,得出的结论为弹道导弹防御系统中地基雷达的部署方式提供了有效的参考依据。%In order to solve the optimal deployment problem of ground-based phased array radar in detecting ballistic targets,the orbit motion and precession motion models of ballistic targets were built up,and the detection probability model for ballistic targets by using several ground-based phased array radars was proposed.Three evaluation indexes of radars'detection performance were given: average detection probability,stable tracking time and resource redundancy time .According to the variation of RCS and detection range for ballistic targets in midcourse,detection performance evaluation indexes of several radar deployment schemes were analyzed through experiments .The conclusion in this paper may provide some reference for deploying the ground-based radar in ballistic missile defense (BMD) system for targets'optimal detection.

  16. 基于多维极化信息的弹道目标综合识别方法%Synthetic recognition method of ballistic targets based on multi-dimensional polarization information

    Institute of Scientific and Technical Information of China (English)

    庞礴; 代大海; 王雪松; 李永祯

    2013-01-01

    目标识别是弹道导弹防御系统的核心难题之一,针对弹道导弹突防过程中无源诱饵的极化识别问题进行了研究.首先,基于多个窄带和宽带极化特征量,并结合暗室测量数据,进行了极化特征提取和优选,去除了冗余的极化特征量.在此基础上,提出了一种基于宽窄带极化特征的弹道目标综合识别方法,并利用弹道目标的暗室实测数据进行了验证.结果表明综合识别方法和仅基于窄带或宽带极化特征的识别方法相比具有更好的目标识别性能.%Target recognition is the core difficulty in ballistic missile defense systems, this paper studies the polarization recognition problem of passive decoy during break through process of the ballistic missile. Firstly, based on a host of narrow and wide band polarization characteristics, and combined with data derived from ane-choic chamber measurement, this paper performs polarization characteristic extraction and filtration, and removes redundant polarization characteristics. A synthetic recognition method based on narrow and wide band polarization characteristics for ballistic targets is proposed, and data derived from anechoic chamber measurement is used for validation. The result shows that the synthetic recognition method has better recognition performance than recognition method based only on narrow or wide band polarization characteristics.

  17. The Truth About Ballistic Coefficients

    CERN Document Server

    Courtney, Michael

    2007-01-01

    The ballistic coefficient of a bullet describes how it slows in flight due to air resistance. This article presents experimental determinations of ballistic coefficients showing that the majority of bullets tested have their previously published ballistic coefficients exaggerated from 5-25% by the bullet manufacturers. These exaggerated ballistic coefficients lead to inaccurate predictions of long range bullet drop, retained energy and wind drift.

  18. Algorithm of reentry ballistic target tracking based on multiple model%基于多模型的再入弹道目标跟踪算法

    Institute of Scientific and Technical Information of China (English)

    钮俊清; 任清安; 刘军伟

    2015-01-01

    In the anti-missile defense system, the tracking and identification of reentry ballistic target are the critical problems. However, the traditional method could not applied to the tracking for different types of reentry ballistic targets and identification of the true or fake warhead. This paper focus on an algorithm of reentry ballistic target tracking based on multiple model. In this scheme, the multiple model configuration is used for tracking the different types of reentry ballistic targets, thus improving the tracking accuracy effectively, and meanwhile, possessing the fast rate of convergence and better precision for the ballistic coefficient estimation. Simulation results indicate that this proposed method improves the precision of target tracking greatly, compared to the conventional EKF algorithm, and has especially a higher precision for the ballistic coefficient estimation and a certain capability of identifying the true or fake warhead and robust tracking performance.%再入弹道导弹目标的跟踪和识别是反导防御体系中最关键的问题。针对传统的跟踪方法不能适用于不同类型的再入弹道目标的跟踪和真假弹头的识别问题,提出一种基于多模型的再入段弹道目标跟踪算法。该算法采用多模型的结构,适用于跟踪不同类型的再入弹道目标,可有效地提高跟踪精度;同时对于弹道系数的估计具有很快的收敛速度和较好的估计精度。仿真结果表明,与传统的EKF算法相比较,本文算法大幅提高了目标跟踪的精度,特别在弹道系数估计上精度较高,具有一定的识别真假弹头的能力和鲁棒的跟踪性能。

  19. 基于多模型的再入弹道目标跟踪算法%Algorithm of reentry ballistic target tracking based on multiple model

    Institute of Scientific and Technical Information of China (English)

    钮俊清; 任清安; 刘军伟

    2015-01-01

    In the anti-missile defense system, the tracking and identification of reentry ballistic target are the critical problems. However, the traditional method could not applied to the tracking for different types of reentry ballistic targets and identification of the true or fake warhead. This paper focus on an algorithm of reentry ballistic target tracking based on multiple model. In this scheme, the multiple model configuration is used for tracking the different types of reentry ballistic targets, thus improving the tracking accuracy effectively, and meanwhile, possessing the fast rate of convergence and better precision for the ballistic coefficient estimation. Simulation results indicate that this proposed method improves the precision of target tracking greatly, compared to the conventional EKF algorithm, and has especially a higher precision for the ballistic coefficient estimation and a certain capability of identifying the true or fake warhead and robust tracking performance.%再入弹道导弹目标的跟踪和识别是反导防御体系中最关键的问题。针对传统的跟踪方法不能适用于不同类型的再入弹道目标的跟踪和真假弹头的识别问题,提出一种基于多模型的再入段弹道目标跟踪算法。该算法采用多模型的结构,适用于跟踪不同类型的再入弹道目标,可有效地提高跟踪精度;同时对于弹道系数的估计具有很快的收敛速度和较好的估计精度。仿真结果表明,与传统的EKF算法相比较,本文算法大幅提高了目标跟踪的精度,特别在弹道系数估计上精度较高,具有一定的识别真假弹头的能力和鲁棒的跟踪性能。

  20. Metamaterials for Ballistic Electrons

    CERN Document Server

    Dragoman, D; Dragoman, Daniela; Dragoman, Mircea

    2007-01-01

    The paper presents a metamaterial for ballistic electrons, which consists of a quantum barrier formed in a semiconductor with negative effective electron mass. This barrier is the analogue of a metamaterial for electromagnetic waves in media with negative electrical permittivity and magnetic permeability. Besides applications similar to those of optical metamaterials, a nanosized slab of a metamaterial for ballistic electrons, sandwiched between quantum wells of positive effective mass materials, reveals unexpected conduction properties, e.g. single or multiple room temperature negative differential conductance regions at very low voltages and with considerable peak-to-valley ratios, while the traversal time of ballistic electrons can be tuned to larger or smaller values than in the absence of the metamaterial slab. Thus, slow and fast electrons, analogous to slow and fast light, occur in metamaterials for ballistic electrons.

  1. Ballistic Test Facility

    Data.gov (United States)

    Federal Laboratory Consortium — The Ballistic Test Facility is comprised of two outdoor and one indoor test ranges, which are all instrumented for data acquisition and analysis. Full-size aircraft...

  2. 15 CFR 742.5 - Missile technology.

    Science.gov (United States)

    2010-01-01

    ... 15 Commerce and Foreign Trade 2 2010-01-01 2010-01-01 false Missile technology. 742.5 Section 742... BASED CONTROLS § 742.5 Missile technology. (a) License requirements. (1) In support of U.S. foreign... establish the existence of a contract. (d) Missile Technology Control Regime. Missile Technology...

  3. Discussion of the target-missile control scheme with supersonic speed at minimum altitude

    Institute of Scientific and Technical Information of China (English)

    2006-01-01

    An antiship missile with supersonic speed at minimum altitude is an effective weapon to break through a defense line. The former Soviet Union was a leader in this field since it had developed several kinds of antiship missiles which obtained supersonic speed at minimum altitudes. To counter this kind of missile,many countries have been developing corresponding antimissiles. For the purpose of verifing the antimissile missile's effectiveness in intercepting antiship missiles, a target-missile is needed. A target-missle is cheaper and can imitate the main characteristics of antiship missiles with supersonic speed at minimum altitude. In this paper, the control scheme of a target missile flying with supersonic speed at minimum altitude is studied. To counter the problem of hedgehopping over the sea, a control scheme utilizing a SINS + altimeter was proposed.In this scheme, both the quick response ability of altitude control and the anti-jamming problem were considered. A simulation experiment shows that when an integrated altitude control system is used, the anti-disturbance ability of the integrated altitude is good and the response speed of altitude control system can be dramatically improved.

  4. Analysis of Energy Dissipation Mechanisms of Woven Fabrics Subjected to Ballistic Impact

    OpenAIRE

    IŞIK, Halil; DEĞİRMENCİ, Ercan; EVCİ, Celal

    2013-01-01

    It is important for combat vehicles and technological defense systems used in the battlefield to be lightweight for maneuverability while they still provide effective protection for survivability. Desired ballistic protection of defense systems may be attained by armor systems developed with different materials. The most important factor in the design of armor is the optimization of ballistic protection/weight ratio. The protection degree needed for sufficient survivability is limited by the ...

  5. Adaptive Missile Guidance Using GPS

    Directory of Open Access Journals (Sweden)

    Pallavi Sharad Rupnar

    2013-05-01

    Full Text Available The name adaptive means we can guide any missile using GPS in any critical conditions. GPS guided missiles, using the exceptional navigational and surveying abilities of GPS, after being launched, could deliver a warhead to any part of the globe via the interface of the onboard computer in the missile with the GPS satellite system.GPS allows accurate targeting of various military weapons including ICBMs, cruise missiles and precision-guided munitions. Artillery projectiles with embedded GPS receivers able to withstand accelerations of 12,000 G have been developed for use in 155mm.GPS guided weapons, with their technological advances over previous, are the superior weapon of choice in modern days

  6. Art in Internal Ballistics

    Directory of Open Access Journals (Sweden)

    K.S. Bhaskara Rao

    1982-04-01

    Full Text Available A review of the computations in Internal Ballistic Systems for developing pressure and velocity space curves, called primary problem and differential variations due to change in initial phase space of loading conditions, called secondary problem, is presented. In the concluding part, the general aspects of the secondary problem are analysed and reported.

  7. Art in Internal Ballistics

    OpenAIRE

    K.S. Bhaskara Rao; Sharma, K. C.

    1982-01-01

    A review of the computations in Internal Ballistic Systems for developing pressure and velocity space curves, called primary problem and differential variations due to change in initial phase space of loading conditions, called secondary problem, is presented. In the concluding part, the general aspects of the secondary problem are analysed and reported.

  8. Analysis on Ship-to-Air Missile Kill ZoneUnder Ship-Ship Coordinate Air Defense%舰舰协同防空的舰空导弹杀伤区分析

    Institute of Scientific and Technical Information of China (English)

    姚跃亭; 赵建军; 刘林密; 崔伟成

    2011-01-01

    In order to describe the coupling kill zone in fleet coordinate air defense quantitatively, the depth and shape of it is studied. The characters of kill zone in single ship air defense is analyzed, the typical formation of fleet air defense is studied, and the hierarchical closed circle theory that hierarchical multi-layer in longitudinal direction and coupled of same order in latitudinal direction is given. According to the zero and none zero airway shortcut, the calculation model of first order coupled kill zone depth is brought forward. And it is extended to higher order. The sensitiveness of spacing interval and azimuth angle to the coupled kill zone depth is simulated. Results show that the model can be instructive.%针对舰艇编队协同防空时的耦合杀伤区形状及纵深等问题进行了研究,以定量地对编队耦合杀伤区进行简化描述.分析了单舰对典型目标的杀伤区特性,探讨了舰艇编队的典型防空队形,研究了纵向上递阶多层次、横向上同阶耦合的"递阶封闭圈原理".以一阶耦合杀伤区为重点,依据攻击目标的不同,将其分成相对航路捷径为零和相对航路捷径均非零两类情况建立了耦合杀伤区纵深的计算模型,并扩展到了高阶耦合的情况.研究了耦合杀伤区与舰舰间距和来袭目标进攻舷角等参数的相互关系以及灵敏度.结果表明建立的模型符合实际,具有一定的指导意义.

  9. Concrete wall perforation by rigid missile

    International Nuclear Information System (INIS)

    Tests were performed to study the perforation risk of reinforced concrete by industrial accidental missile. An empiric formula is established from shots of cylindrical missile with flat nose and its validity range is set. Some shots with different missile shape have given correction to introduce then in the formula. Calculation with finite elements are compared with tests results

  10. Baseline marine biological survey at the Peacock Point outfall and other point-source discharges on Wake Atoll, Pacific Ocean in 1998-06 (NODC Accession 0000247)

    Data.gov (United States)

    National Oceanic and Atmospheric Administration, Department of Commerce — The U.S. Army Space and Missile Defense Command (SMDC) in support of the Ballistic Missile Defense Organization (BMDO) sponsored a marine biological survey at Wake...

  11. Marine Biological Survey, Peacock Point Outfall, Wake Atoll June 1998 (NODC Accession 0000247)

    Data.gov (United States)

    National Oceanic and Atmospheric Administration, Department of Commerce — The U.S. Army Space and Missile Defense Command (SMDC), in support of the Ballistic Missile Defense Organization (BMDO) sponsored a marine biological survey at Wake...

  12. Survivability Armor Ballistic Laboratory (SABL)

    Data.gov (United States)

    Federal Laboratory Consortium — The SABL provides independent analysis, ballistic testing, data collection, data reduction and qualification of current and advanced armors. Capabilities: The SABL...

  13. Robust missile feedback control strategies

    NARCIS (Netherlands)

    Trottemant, E.J.; Scherer, C.W.; Weiss, M.; Vermeulen, A.

    2010-01-01

    The nature of the missile interception problem with two noncooperative players leads to the field of differential games. Introducing nonlinear uncertain models can potentially lead to nonexistence of game theoretic equilibrium strategies, computationally intractable problems, and/or highly reduced p

  14. Missile impact on structural members

    International Nuclear Information System (INIS)

    In this paper, a unified methodology will be developed to evaluate impact effects of hard missiles on reinforced concrete and steel members including plates/walls and beams. The solution will be investigated based on two ultimate limit states: local perforation and structural collapse of flexible plates and beams

  15. Generation of missiles by tornadoes

    International Nuclear Information System (INIS)

    Available data on tornado wind velocities and wind distribution are incorporated into a mathematical model of the tornado wind field. The mathematical model is then used to predict the time-history of motion of a potential missile in a tornado wind field. (U.S.)

  16. Trajectory Optimization Design for Morphing Wing Missile

    Institute of Scientific and Technical Information of China (English)

    Ruisheng Sun; Chao Ming; Chuanjie Sun

    2015-01-01

    This paper presents a new particle swarm optimization ( PSO) algorithm to optimize the trajectory of morphing⁃wing missile so as to achieve the enlargement of the maximum range. Equations of motion for the two⁃dimensional dynamics are derived by treating the missile as an ideal controllable mass point. An investigation of aerodynamic characteristics of morphing⁃wing missile with varying geometries is performed. After deducing the optimizing trajectory model for maximizing range, a type of discrete method is put forward for taking optimization control problem into nonlinear dynamic programming problem. The optimal trajectory is solved by using PSO algorithm and penalty function method. The simulation results suggest that morphing⁃wing missile has the larger range than the fixed⁃shape missile when launched at supersonic speed, while morphing⁃wing missile has no obvious range increment than the fixed⁃shape missile at subsonic speed.

  17. Tornado-borne missile speeds. Final report

    International Nuclear Information System (INIS)

    An investigation of the question of tornado-borne missile speeds was carried out, with a view to identify pertinent areas of uncertainty and to estimate credible tornado-borne missile speeds - within the limitations inherent in the present state of the art. The investigation consists of two parts: (1) a study in which a rational model for the missile motion is proposed, and numerical experiments are carried out corresponding to various assumptions on the initial conditions of the missile motion, the structure of the tornado flow, and the aerodynamic properties of the missile; (2) a theoretical and experimental study of tornado-borne missile aerodynamics, conducted by Colorado State Univ. (CSU) to be covered in a separate report by CSU. In the present report, the factors affecting missile motion and their influence upon such motion are examined

  18. Countermeasure effectiveness against an intelligent imaging infrared anti-ship missile

    Science.gov (United States)

    Gray, Greer J.; Aouf, Nabil; Richardson, Mark; Butters, Brian; Walmsley, Roy

    2013-02-01

    Ship self defense against heat-seeking anti-ship missiles is of great concern to modern naval forces. One way of protecting ships against these threats is to use infrared (IR) offboard countermeasures. These decoys need precise placement to maximize their effectiveness, and simulation is an invaluable tool used in determining optimum deployment strategies. To perform useful simulations, high-fidelity models of missiles are required. We describe the development of an imaging IR anti-ship missile model for use in countermeasure effectiveness simulations. The missile model's tracking algorithm is based on a target recognition system that uses a neural network to discriminate between ships and decoys. The neural network is trained on shape- and intensity-based features extracted from simulated imagery. The missile model is then used within ship-decoy-missile engagement simulations, to determine how susceptible it is to the well-known walk-off seduction countermeasure technique. Finally, ship survivability is improved by adjusting the decoy model to increase its effectiveness against the tracker.

  19. Applications of the Continuous Acquisition and Life-cycle Support (CALS) initiative to the evolved SEASAPPROW Missile program

    OpenAIRE

    Fuhs, Hans Georg

    1995-01-01

    This thesis reviews the Continuous Acquisition and Life-cycle Support (CALS) initiative and its data format specifications and analyzes how they were applied to the Evolved SEASPARROW Missile (ES SM) Program. The CALS initiative and its data format specifications were developed to facilitate management of defense system technical data. With recent reforms in defense acquisition policy called for in Secretary of Defense memorandum, "Specifications & Standards - A New Way of Doing Business" the...

  20. Ballistic quality assurance

    International Nuclear Information System (INIS)

    This review describes the ballistic quality assurance for stereotactic intracranial irradiation treatments delivered with Gamma KnifeR either dedicated or adapted medical linear accelerators. Specific and periodic controls should be performed in order to check the mechanical stability for both irradiation and collimation systems. If this step remains under the responsibility of the medical physicist, it should be done in agreement with the manufacturer's technical support. At this time, there are no recent published guidelines. With technological developments, both frequency and accuracy should be assessed in each institution according to the treatment mode: single versus hypo-fractionated dose, circular collimator versus micro-multi-leaf collimators. In addition, 'end-to-end' techniques are mandatory to find the origin of potential discrepancies and to estimate the global ballistic accuracy of the delivered treatment. Indeed, they include frames, non-invasive immobilization devices, localizers, multimodal imaging for delineation and in-room positioning imaging systems. The final precision that could be reasonably achieved is more or less 1 mm. (authors)

  1. Analyzing and designing object-oriented missile simulations with concurrency

    Science.gov (United States)

    Randorf, Jeffrey Allen

    2000-11-01

    A software object model for the six degree-of-freedom missile modeling domain is presented. As a precursor, a domain analysis of the missile modeling domain was started, based on the Feature-Oriented Domain Analysis (FODA) technique described by the Software Engineering Institute (SEI). It was subsequently determined the FODA methodology is functionally equivalent to the Object Modeling Technique. The analysis used legacy software documentation and code from the ENDOSIM, KDEC, and TFrames 6-DOF modeling tools, including other technical literature. The SEI Object Connection Architecture (OCA) was the template for designing the object model. Three variants of the OCA were considered---a reference structure, a recursive structure, and a reference structure with augmentation for flight vehicle modeling. The reference OCA design option was chosen for maintaining simplicity while not compromising the expressive power of the OMT model. The missile architecture was then analyzed for potential areas of concurrent computing. It was shown how protected objects could be used for data passing between OCA object managers, allowing concurrent access without changing the OCA reference design intent or structure. The implementation language was the 1995 release of Ada. OCA software components were shown how to be expressed as Ada child packages. While acceleration of several low level and other high operations level are possible on proper hardware, there was a 33% degradation of 4th order Runge-Kutta integrator performance of two simultaneous ordinary differential equations using Ada tasking on a single processor machine. The Defense Department's High Level Architecture was introduced and explained in context with the OCA. It was shown the HLA and OCA were not mutually exclusive architectures, but complimentary. HLA was shown as an interoperability solution, with the OCA as an architectural vehicle for software reuse. Further directions for implementing a 6-DOF missile modeling

  2. Electro-chemical batteries for guided missiles

    Directory of Open Access Journals (Sweden)

    H. S. Jaggi

    1966-05-01

    Full Text Available Electro-chemical batteries owing to their simplicity and ease of stowage form one of the sources of electrical power inside a missile. However, all batteries are not suited for this application. This article describes the special features required of a missile borne battery pack and discusses the characteristics of various types of batteries available today in the world. Conclusions have been drawn as to the most suitable types of batteries for missile applications.

  3. Beyond the cold war nuclear legacy: offense-defense and the role of nuclear deterrence

    International Nuclear Information System (INIS)

    Since the September 11 terrorist attacks on the World Trade Center and the Pentagon, the defense community of the United States focused overwhelmingly on countering the threat of global terrorism. This focus rightly reflects the danger of additional terrorist attacks against the American homeland, including conceivably even with nuclear weapons or radiological devices. At the same time, the December, 2001 announcement of the U.S. decision to withdraw from the 1972 Anti-Ballistic Missile (ABM) Treaty after the six month waiting period serves as a reminder that there still is considerable other outstanding 'defense business' confronting the United States and its European allies. In particular, it is increasingly essential to re-craft the Cold War nuclear weapons legacy, not only in its own right but because doing so can also have important payoffs for the success of the U.S.-led global anti-terrorist campaign. The following paper first describes some of the main features of the Cold War nuclear legacy. It then sketches a number of different schools of thought or camps that exist within the U.S. defense community in answer to the question, 'what next with nuclear weaponry?' In light of those contending positions, it then sets out a possible way ahead - moving to re-craft U.S. strategic dealings with Russia toward a non-adversary relationship, to avoid a new Cold War with China, and to put in place the right mix of offensive and defensive, nuclear and non-nuclear capabilities to contain 21. century proliferation dangers. (author)

  4. Beyond the cold war nuclear legacy: offense-defense and the role of nuclear deterrence

    Energy Technology Data Exchange (ETDEWEB)

    Dunn, L.A

    2001-07-01

    Since the September 11 terrorist attacks on the World Trade Center and the Pentagon, the defense community of the United States focused overwhelmingly on countering the threat of global terrorism. This focus rightly reflects the danger of additional terrorist attacks against the American homeland, including conceivably even with nuclear weapons or radiological devices. At the same time, the December, 2001 announcement of the U.S. decision to withdraw from the 1972 Anti-Ballistic Missile (ABM) Treaty after the six month waiting period serves as a reminder that there still is considerable other outstanding 'defense business' confronting the United States and its European allies. In particular, it is increasingly essential to re-craft the Cold War nuclear weapons legacy, not only in its own right but because doing so can also have important payoffs for the success of the U.S.-led global anti-terrorist campaign. The following paper first describes some of the main features of the Cold War nuclear legacy. It then sketches a number of different schools of thought or camps that exist within the U.S. defense community in answer to the question, 'what next with nuclear weaponry?' In light of those contending positions, it then sets out a possible way ahead - moving to re-craft U.S. strategic dealings with Russia toward a non-adversary relationship, to avoid a new Cold War with China, and to put in place the right mix of offensive and defensive, nuclear and non-nuclear capabilities to contain 21. century proliferation dangers. (author)

  5. Missile Design PC TRAP: an improved PC TRAP for tactical missile design

    OpenAIRE

    Gibeau, Daniel G.

    1993-01-01

    Approved for public release; distribution is unlimited. The Missile Design Personal Computer Trajectory Analysis Program (Missile Design PCTRAP) is a simple and compact multi-purpose tactical missile simulation program that runs quickly on any IBM-compatible personal computer. It is an improved version of the Captain, Canadian Air Force

  6. Application of IPAD to missile design

    Science.gov (United States)

    Santa, J. E.; Whiting, T. R.

    1974-01-01

    The application of an integrated program for aerospace-vehicle design (IPAD) to the design of a tactical missile is examined. The feasibility of modifying a proposed IPAD system for aircraft design work for use in missile design is evaluated. The tasks, cost, and schedule for the modification are presented. The basic engineering design process is described, explaining how missile design is achieved through iteration of six logical problem solving functions throughout the system studies, preliminary design, and detailed design phases of a new product. Existing computer codes used in various engineering disciplines are evaluated for their applicability to IPAD in missile design.

  7. Infrared Background and Missiles Signature Survey

    Directory of Open Access Journals (Sweden)

    D.V. Renuka

    2013-12-01

    Full Text Available The proliferation of the missile threats in the existing threat scenario for airborne platform is a serious point of consideration for any mission planning. Missile warning system is an electronic warfare support system which gives warning to the pilot when a missile is detected in the scenario. The airborne platform has to be installed with missile warning sensors to give a spherical coverage, so that the sensors can detect the IR intensity variation in the ground scenario. This IR intensity variation has to be further analysed to differentiate the raising missile intensity from the varying background clutter. In order to differentiate the threat from the background clutter, the system should have sufficient background data set for online comparison thereby having less false alarm rate. The efficiency and performance of any missile warning system is validated with respect to its probability of declaration against the false alarm rate. Hence, to realize an efficient functioning of missile warning system, building IR background data base and missile signature database are the primary task. This paper details the methodology to be adapted for the building of tactical missile IR signatures and background data.Defence Science Journal, 2013, 63(6, pp.611-615, DOI:http://dx.doi.org/10.14429/dsj.63.5762

  8. Infrared Background and Missiles Signature Survey

    Directory of Open Access Journals (Sweden)

    D.V. Renuka

    2013-11-01

    Full Text Available The proliferation of the missile threats in the existing threat scenario for airborne platform is a serious point of consideration for any mission planning. Missile warning system is an electronic warfare support system which gives warning to the pilot when a missile is detected in the scenario. The airborne platform has to be installed with missile warning sensors to give a spherical coverage, so that the sensors can detect the IR intensity variation in the ground scenario. This IR intensity variation has to be further analysed to differentiate the raising missile intensity from the varying background clutter. In order to differentiate the threat from the background clutter, the system should have sufficient background data set for online comparison thereby having less false alarm rate. The efficiency and performance of any missile warning system is validated with respect to its probability of declaration against the false alarm rate. Hence, to realize an efficient functioning of missile warning system, building IR background data base and missile signature database are the primary task. This paper details the methodology to be adapted for the building of tactical missile IR signatures and background data.

  9. A Direct Interception Missile Assignment Model in Firepower Planning of Double-Layer Anti-Missile Combat%直接分配到弹的双层反导火力规划模型

    Institute of Scientific and Technical Information of China (English)

    李龙跃; 刘付显; 杨国哲; 赵麟锋

    2014-01-01

    Firepower application is one of the core problem in anti-missile power construction,Firepower Planning of double-layer anti-missile combat in terminal phase is a Nondeterministic polynomial hard Mod-eling question.We analysis the problem,when to assign the interception missiles to the targets and give the model assumptions;Then we establish the direct interception missile assignment model in firepower planning of double-layer anti-missile combat This model break the research which targets only can be as-signed to the weapon system or fire units in the past,assigned the interception missiles to ballistic missiles one by one,it's a new idea about firepower planning.%反导作战火力运用是反导力量建设的核心内容之一,末段双层反导火力规划是一个复杂的不确定多约束条件优化问题,对火力规划进行了问题分析、弹-目分配时机分析和模型假设;分2个阶段建立了直接分配到弹的末段双层反导火力规划模型,模型重点考虑拦截目标与拦截弹杀伤时间窗口的对应关系,建立起武器系统拦截弹与来袭目标的弹-目对应分配关系,提供一种新的、快速的双层反导火力规划方法。

  10. [Terminal ballistics. 3].

    Science.gov (United States)

    Marini, F; Mangiante, G; Dagradi, V; Radin, S; Carolo, F; Giarolli, M; Della Giacoma, G; Tosi, D; Merico, G; Tenci, A

    1993-01-01

    This brief chapter, focusing essentially on a single topic, has been written in homage to Emile Theodor Kocker, a masterful exponent of the art of surgery and founder of the culture of terminal ballistics. For most of the literature we are indebted to Fackler and Dougherty, who, with the particular grasp, and fair of historians, act as guides on a trial which is only apparently retrograde, but which actually bears eloquent witness to the fact that even in the most physically tangible of arts, namely the art of surgery, inspired curiosity may help us to go well beyond the limits of our day and age. This chapter is also dedicated to the memory of another great surgeon, Vittorio Pettinari, who for one of the authors was an incomparable mentor and past-master of such curiosity. PMID:7923495

  11. Cooperative Monitoring Center Occasional Paper/4: Missile Control in South Asia and the Role of Cooperative Monitoring Technology

    Energy Technology Data Exchange (ETDEWEB)

    Kamal, N.; Sawhney, P.

    1998-10-01

    The succession of nuclear tests by India and Pakistan in May 1998 has changed the nature of their missile rivalry, which is only one of numerous manifestations of their relationship as hardened adversaries, deeply sensitive to each other's existing and evolving defense capabilities. The political context surrounding this costly rivalry remains unmediated by arms control measures or by any nascent prospect of detente. As a parallel development, sensible voices in both countries will continue to talk of building mutual confidence through openness to avert accidents, misjudgments, and misinterpretations. To facilitate a future peace process, this paper offers possible suggestions for stabilization that could be applied to India's and Pakistan's missile situation. Appendices include descriptions of existing missile agreements that have contributed to better relations for other countries as well as a list of the cooperative monitoring technologies available to provide information useful in implementing subcontinent missile regimes.

  12. Tornado missiles protections taken at the Ikata NPP of SEPCO

    International Nuclear Information System (INIS)

    On July 8, 2013, the new regulatory requirements for commercial power reactors got in force. Based on a concept of 'Defense-in-depth', essential importance was placed on the third and fourth layers of defense and prevention of simultaneous loss of all safety functions due to common causes. In this regards, the previous assumptions on the impact of earthquakes, tsunamis and other external events such as volcanic eruptions, tornadoes and forest fires were re-evaluated, and countermeasures for nuclear safety against these external events were decided to be enhanced. For tornado, Nuclear Regulation Authority promulgated the 'Assessment Guide for Tornado Effect on Nuclear Power Plants' to evaluate the effect of tornadoes. This paper will introduce the outline of evaluation cases of tornado effect, and tornado missiles protections taken at the Ikata Unit 3 Nuclear Power Plant (for actual case studies). (author)

  13. 77 FR 51970 - Renewal of Missile Defense Advisory Committee

    Science.gov (United States)

    2012-08-28

    ... no voting rights. Non-voting experts and consultants shall serve terms of appointments as determined... representing any particular point of view and in a manner that is free from conflict of interest....

  14. Army Air and Missile Defense Network Design Facility (AAMDNDF)

    Data.gov (United States)

    Federal Laboratory Consortium — This facility provides JTIDS network designs and platform initialization load files for all Joint and Army-only tests, exercises, operations, and contingency events...

  15. Ballistic studies on layered structures

    International Nuclear Information System (INIS)

    This paper presents the ballistic behavior and penetration mechanism of metal-metal and metal-fabric layered structures against 7.62 armour piercing projectiles at a velocity of 840 ± 15 m/s at 30o angle of impact and compares the ballistic results with that of homogeneous metallic steel armour. This study also describes the effect of keeping a gap between the target layers. Experimental results showed that among the investigated materials, the best ballistic performance was attained with metal-fabric layered structures. The improvements in ballistic performance were analyzed in terms of mode of failure and fracture mechanisms of the samples by using optical and electron microscope, X-ray radiography and hardness measurement equipments.

  16. Internal Ballistics of Recoilless Guns

    Directory of Open Access Journals (Sweden)

    Asim Ray

    1967-01-01

    Full Text Available A new method for calculating the ballistics of recoilless guns during the period of burning of the propellant has been obtained. Ballistics have also been calculated by exact numerical integration in a few cases and these results have been compared with those obtained by the method described in this paper. It has been found that the results obtained by these two methods agree satisfactorily.

  17. Software design of missile integrated test system

    Science.gov (United States)

    Dai, Jing; Zhang, Ping; Li, Xingshan; Liao, Canxing; Wang, Zongli

    2006-11-01

    Based on virtual instrument, software design precept of missile integrated test system is proposed in this paper. The integrated test system software was developed under modular, intelligent and structured precept. In this way, the expansion capability of the test software is improved, and it is very convenient for second-development and maintenance. This test software is of higher-degree automation, its integrated test environment gives full play to the hardware platform of the missile integrated test system. In response to the specific hardware configuration of the test system and special missile test requirements, the application of test resources was optimized in the test procedure to improve test speed greatly and satisfy the power-on time limit for missile test. At the same time, by applying multithreading and hardware clock on a data acquisition card, accurate data acquisition, data calculating and data injecting can be completed in a millisecond to satisfy the harsh missile test requirement. This automatic test equipment can automatically test the nose cabin and control cabin only of a missile and a training missile; all the missile test items can be accomplished in a short period of time to enhance the efficiency and reliability of the test.

  18. Principles of Guided Missiles and Nuclear Weapons.

    Science.gov (United States)

    Naval Personnel Program Support Activity, Washington, DC.

    Fundamentals of missile and nuclear weapons systems are presented in this book which is primarily prepared as the second text of a three-volume series for students of the Navy Reserve Officers' Training Corps and the Officer Candidate School. Following an introduction to guided missiles and nuclear physics, basic principles and theories are…

  19. Use of noise attenuation modeling in managing missile motor detonation activities.

    Science.gov (United States)

    McFarland, Michael J; Watkins, Jeffrey W; Kordich, Micheal M; Pollet, Dean A; Palmer, Glenn R

    2004-03-01

    The Sound Intensity Prediction System (SIPS) and Blast Operation Overpressure Model (BOOM) are semiempirical sound models that are employed by the Utah Test and Training Range (UTTR) to predict whether noise levels from the detonation of large missile motors will exceed regulatory thresholds. Field validation of SIPS confirmed that the model was effective in limiting the number of detonations of large missile motors that could potentially result in a regulatory noise exceedance. Although the SIPS accurately predicted the impact of weather on detonation noise propagation, regulators have required that the more conservative BOOM model be employed in conjunction with SIPS in evaluating peak noise levels in populated areas. By simultaneously considering the output of both models, in 2001, UTTR detonated 104 missile motors having net explosive weights (NEW) that ranged between 14,960 and 38,938 lb without a recorded public noise complaint. Based on the encouraging results, the U.S. Department of Defense is considering expanding the application of these noise models to support the detonation of missile motors having a NEW of 81,000 lb. Recent modeling results suggest that, under appropriate weather conditions, missile motors containing up to 96,000 lb NEW can be detonated at the UTTR without exceeding the regulatory noise limit of 134 decibels (dB).

  20. Discrete Deterministic Modelling of Autonomous Missiles Salvos

    Directory of Open Access Journals (Sweden)

    Momcilo Milinovic

    2014-09-01

    Full Text Available The paper deals with mathematical models of sequent salvos battle, of autonomous flight missiles (AFM organized in the groups of combatants. Tactical integration of AFM system distance-controlled weapon is considered by performances of simultaneous approaches on targets, and continual battle models of guerilla and direct fire, are redesigned to the discrete-continual mixed model, for checking missiles sudden, and further salvos, attack effects. Superiority parameters, as well as losses and strengths of full, or the part of salvo battle, for the missiles groups as technology sub-systems combatants’, is expressed by mathematical and simulation examples. Targets engagements capacities of the missiles battle unit, is conducted through designed scenarios and mathematically derived in the research. Model orientated on answers about employment of rapid reaction defending tactics, by distance missiles attacks.Defence Science Journal, Vol. 64, No. 5, September 2014, pp.471-476, DOI:http://dx.doi.org/10.14429/dsj.64.5791

  1. Impact load for tornado-generated missiles

    International Nuclear Information System (INIS)

    Nuclear power plant structures are designed to resist impact loads from tornado-generated missiles. The paper gives a method to determine the contact pressure at the interface of the missile and the target, and the velocity and deceleration time-histories of the missile. It also gives a method to obtain the design load due to impact by tornado-generated missiles. The calculated design load compares very well with the total support reaction from a full-scale dynamics test. The comparison between the predicted deceleration and the deceleration recorded in a test is excellent. The method of determining the deceleration has also been used with very good results for earth-penetrating missiles. (Auth.)

  2. Analysis of Rocket, Ram-Jet, and Turbojet Engines for Supersonic Propulsion of Long-Range Missles. II - Rocket Missile Performance

    Science.gov (United States)

    Huff, Vearl N.; Kerrebrock, Jack

    1954-01-01

    The theoretical performance of a two-stage ballistic rocket mis having a centerbody and two parallel boosters was investigated for J oxygen and ammonia-fluorine propellants. Both power-plant and missi parameters were optimized to give minimum cost on-the basis of the analysis for a range of 5500 nautical miles. After optimum values were found, each parameter was varied independently to determine its effect on performance of the missile. The missile using the ammonia-fluorine propellant weighs about one half as much as a missile using JP4-oxygen. Based on an expected unit cost of fluorine in quantity production, the ammonia-fluorine missile has a substantially lower relative cost than a JP4-oxygen missile. Optimum chamber pressures for both propellant systems and for both the centerbody and boosters were between 450 and 600 pounds per square inch. High design altitudes for the exhaust nozzle are desirable for both the centerbody and boosters. For the centerbody, the design altitude should be between 45,000 and 60,000 feet, with the value for ammonia-fluorine lower than that for JP4-oxygen. For the boosters, the design altitude should be 20,000 to 30,000 feet, with the value for the ammonia-fluorine. missile higher.

  3. [Terminal ballistics. 1].

    Science.gov (United States)

    Mangiante, G; Dagradi, V; Radin, S; Carolo, F; Giarolli, M; Tenci, A; Merico, G; Tosi, D; Acerbi, A; Della Giacoma, G

    1993-01-01

    We have chosen to conceive of terminal ballistics as a violent and extremely rapid confrontation between two forms of resistance before the final state of rest is reached. This definition, which cannot help but don the admittedly loud and outlandish garb of physics, is the most promising for the purposes of biological interpretation. The main characters on this stage are two, but only one of these really plays the lead, namely the human target, which acts out the basic roles inherent in its physical make-up; the other, the bullet, remains a background figure, frozen in its walk-on part, and ready for the next performance. This modus operandi, which is no simplification, but rather an academic necessity, enables us to focus on images which stand out more clearly as a result of an intensive macroscopic spotlight which brings out the features of the individual phenomena, broken down into a succession of close-ups, and subtracts them from the cold physical nature of this or that form of inert matter, which here is merely an occasional, disagreeable witness, or even more, a standing from time to time for but one of the infinite facets of the biological composite being. Here, then, faced with a kind of exploded macrophotograph of a complex kaleidoscope, we see the animal universe, of which we capture so far the plasticity, the subdivisibility, the anisotropy and the cavitation. PMID:7923493

  4. 33 CFR 334.1130 - Pacific Ocean, Western Space and Missile Center (WSMC), Vandenberg AFB, Calif.; danger zones.

    Science.gov (United States)

    2010-07-01

    ... Missile Center (WSMC), Vandenberg AFB, Calif.; danger zones. 334.1130 Section 334.1130 Navigation and Navigable Waters CORPS OF ENGINEERS, DEPARTMENT OF THE ARMY, DEPARTMENT OF DEFENSE DANGER ZONE AND..., Calif.; danger zones. (a) The Area. (1) The waters of the Pacific Ocean in an area extending...

  5. 75 FR 62173 - Bureau of Political-Military Affairs: Directorate of Defense Trade Controls; Notifications to the...

    Science.gov (United States)

    2010-10-07

    ...-production support of the AN/ALQ-131(V) Electronic Countermeasures (``ECM'') System for the Japan Air Self... technical data, and defense services for the manufacture of Patriot PAC-3 Missile Segment Canister... services for the manufacture of PAC-3 Missile Segment Command and Launch System for the Japanese...

  6. Air Drag Effects on the Missile Trajectories

    Directory of Open Access Journals (Sweden)

    F. A. Abd El-Salam

    2011-01-01

    Full Text Available The equations of motion of a missile under the air drag effects are constructed. The modified TD88 is surveyed. Using Lagrange's planetary equations in Gauss form, the perturbations, due to the air drag in the orbital elements, are computed between the eccentric anomalies of the burn out and the reentry points [Ebo,2π−Ebo], respectively. The range equation is expressed as an infinite series in terms of the eccentricity e and the eccentric anomaly E. The different errors in the missile-free range due to the drag perturbations in the missile trajectory are obtained.

  7. Supersonic aerodynamic trade data for a low-profile monoplanar missile concept. [air launched maneuvering missile design

    Science.gov (United States)

    Graves, E. B.; Robins, A. W.

    1979-01-01

    A monoplanar missile concept has been studied which shows promise of improving the aerodynamic performance of air-launched missiles. This missile concept has a constant eccentricity elliptical cross-section body. Since current guidance and propulsion technologies influence missile nose and base shapes, an experimental investigation has been conducted at Mach number 2.50 to determine the effects of variations in these shapes on the missile aerodynamics. Results of these tests are presented.

  8. Tornado missile simulation and risk analysis

    International Nuclear Information System (INIS)

    Mathematical models of the contributing events to the tornado missile hazard at nuclear power plants have been developed in which the major sources of uncertainty have been considered in a probabilistic framework. These models have been structured into a sequential event formalism which permits the treatment of both single and multiple missile generation events. A simulation computer code utilizing these models has been developed to obtain estimates of tornado missile event likelihoods. Two case studies have been analyzed; the results indicate that the probability of a single missile from the sampling population impacting any of the plant's targets is less then about 10-7 per reactor-year. Additional work is needed for verification and sensitivity study

  9. Quality and Reliability of Missile System

    Directory of Open Access Journals (Sweden)

    Mr. Prahlada

    2002-01-01

    Full Text Available Missile system is a single-shot weapon system which requires very high quality and reliability. Therefore, quality and reliability have to be built into the system from designing to testing and evaluation. In this paper, the technological challenges encountered during development of operational missile system and the factors considered to build quality and reliability through the design, manufacture, assembly, testing and by sharing the knowledge with other aerospace agencies, industries and institutions, etc. have been presented.

  10. Tactical and Strategic Missile Technology and Design

    OpenAIRE

    Brophy, Christopher; Healey, Anthony

    2008-01-01

    This brochure explains the Tactical and Strategic Missile Technology and Design program at the Naval Postgraduate School. Sections include: An introduction, description of courses, NPS faculty, research facilities, students eligible, application process, and tuition. The department of Mechanical and Astronautical Engineering offers a missile systems engineering track within the framework of a Master’s Degree in Mechanical Engineering. The program allows students to take courses...

  11. Anti-aircraft Missiles and Gun Control

    OpenAIRE

    BLOCK, Walter

    2016-01-01

    Abstract. Gun control is a highly debatable topic both in the popular and scholarly media. But what about anti-aircraft missiles? Should they be banned? On the one hand, there are fewer of them around, so their challenge is more tractable. On the other hand, they can do far more damage than handguns. The present paper is an attempt to wrestle with this challenge.Keywords. Gun control, Second amendment, Libertarianism, Anti-aircraft missiles.JEL. K15.

  12. Missile non-proliferation: an alternative approach

    International Nuclear Information System (INIS)

    In this report, the author first proposes an overview of the notion of missile prohibition. He notices that the association between weapons of mass destruction and missiles is a prelude to the legitimacy of missile control, notably within the framework of the Missile Technology Control Regime or MTCR. He also comments the notion of total ban. In a second part, the author analyses and discusses the limitations of the control of technology diffusion. He discusses the role of the MTCR, comments the evolution of this regime with the taking of China and Russia into consideration, the impacts of national implementations of export regimes on the MTCR, and economic aspects of control implementation. In the next part, the author addresses other kinds of limitations, i.e. those related with capacity evolutions of proliferating States. The last part addresses the evolution towards a new definition of approach to missile non-proliferation, notably in terms of perception of missile roles and of technology transfer controls

  13. Ballistics examination of air rifle

    OpenAIRE

    Grzegorz Bogiel

    2014-01-01

    The aim of this paper is to determine the velocity, energy, maximum range and distance at which pellets fired from an air rifle of kinetic energy below 17 J can pose a threat to unprotected human skin. Doppler radar equipment and exterior ballistics software were used in this examination.

  14. Ballistics examination of air rifle

    Directory of Open Access Journals (Sweden)

    Grzegorz Bogiel

    2014-08-01

    Full Text Available The aim of this paper is to determine the velocity, energy, maximum range and distance at which pellets fired from an air rifle of kinetic energy below 17 J can pose a threat to unprotected human skin. Doppler radar equipment and exterior ballistics software were used in this examination.

  15. Variable centroid control scheme over hypersonic tactical missile

    Institute of Scientific and Technical Information of China (English)

    易彦; 周凤岐

    2003-01-01

    This paper presents a brand-new tactical missile control scheme--variable centroid vector control according to the international highlight in the field of missile control and the research status of hypersonic missile control in China. Four critical problems related with the new control method are included: improving phase control in the spinning missile single-channel control; establishing variable centroid controlled spinning missile attitude dynamics equations; analyzing variable centroid control strategies and analyzing the stability of the controlled missile and implementing robust control. The achievements and results obtained are valuable and helpful to the theoretical explorations and engineering applications.

  16. Influence of Missile Fusillade Engagement Mode on Operation Efficiency

    Institute of Scientific and Technical Information of China (English)

    BU Xian-jin; REN Yi-guang; SHA Ji-chang

    2008-01-01

    Shoot efficiency is one of the most important evaluation indexes of the operation efficiency of weapon system. In this paper, based on definitions of the probability and the expected number of missed attacking missiles, the expected numbers of anti-missiles and attacking missiles hit by single anti-missile, fusillade mechanism of multi-missile is analyzed systematically. The weapon operation efficiency in various engagement patterns is also studied. The results show that double missiles fusillade is the most feasible manner for increasing the weapon operation efficiency.

  17. Impact load time histories for viscoelastic missiles

    International Nuclear Information System (INIS)

    Generation of the impact load time history at the contact point between a viscoelastic missile and its targets is presented. In the past, in the case of aircraft striking containment shell structure, the impact load history was determined on the basis of actual measurements by subjecting a rigid wall to aircraft crash. The effects of elastic deformation of the target upon the impact load time history is formulated in this paper. The missile is idealized by a linear mass-spring-dashpot combination using viscoelastic models. These models can readily be processed taking into account the elastic as well as inelastic deformations of the missiles. The target is assumed to be either linearly elastic or rigid. In the case of the linearly elastic target, the normal mode theory is used to express the time-dependent displacements of the target which is simulated by lumped masses, elastic properties and dashpots in discrete parts. In the case of Maxwell viscoelastic model, the time-dependent displacements of the missile and the target are given in terms of the unknown impact load time history. This leads to an integral equation which may be solved by Laplace transformation. The normal mode theory is provided. Examples are given for bricks with viscoelastic materials as missiles against a rigid target. (Auth.)

  18. Constrained ballistics and geometrical optics

    OpenAIRE

    Epstein, Marcelo

    2014-01-01

    The problem of constant-speed ballistics is studied under the umbrella of non-linear non-holonomic constrained systems. The Newtonian approach is shown to be equivalent to the use of Chetaev's rule to incorporate the constraint within the initially unconstrained formulation. Although the resulting equations are not, in principle, obtained from a variational statement, it is shown that the trajectories coincide with those of geometrical optics in a medium with a suitably chosen refractive inde...

  19. Reference ballistic imaging database performance.

    Science.gov (United States)

    De Kinder, Jan; Tulleners, Frederic; Thiebaut, Hugues

    2004-03-10

    Ballistic imaging databases allow law enforcement to link recovered cartridge cases to other crime scenes and to firearms. The success of these databases has led many to propose that all firearms in circulation be entered into a reference ballistic image database (RBID). To assess the performance of an RBID, we fired 4200 cartridge cases from 600 9mm Para Sig Sauer model P226 series pistols. Each pistol fired two Remington cartridges, one of which was imaged in the RBID, and five additional cartridges, consisting of Federal, Speer, Winchester, Wolf, and CCI brands. Randomly selected samples from the second series of Remington cartridge cases and from the five additional brands were then correlated against the RBID. Of the 32 cartridges of the same make correlated against the RBID, 72% ranked in the top 10 positions. Likewise, of the 160 cartridges of the five different brands correlated against the database, 21% ranked in the top 10 positions. Generally, the ranking position increased as the size of the RBID increased. We obtained similar results when we expanded the RBID to include firearms with the same class characteristics for breech face marks, firing pin impressions, and extractor marks. The results of our six queries against the RBID indicate that a reference ballistics image database of new guns is currently fraught with too many difficulties to be an effective and efficient law enforcement tool.

  20. On the ballistic response of comminuted ceramics

    International Nuclear Information System (INIS)

    Recent results have strongly suggested that the ballistic-resistance of different comminuted ceramics is similar, independent of the original strength of the material. In particular, experimental work focused on the ballistic response of such materials has suggested that ballistic response is largely controlled by shattered material morphology. Consequently, it has been postulated that control of the nature of ceramic fragmentation should provide a potential route to optimise post-impact ballistic resistance. In particular, such an approach would open up a route to control in multi-hit capabilities. Here, ballistic tests into pre-formed 'fragmented-ceramic' analogues assembled from compacted alumina powders with two differing morphologies were conducted. Strong hints of a morphology-based contribution to ballistic resistance were apparent, although there was insufficient fidelity in the experimental data set to categorically identify the nature of this contribution.

  1. The probability of a tornado missile hitting a target

    International Nuclear Information System (INIS)

    It is shown that tornado missile transportation is a diffusion Markovian process. Therefore, the Green's function method is applied for the estimation of the probability of hitting a unit target area. This propability is expressed through a joint density of tornado intensity and path area, a probability of tornado missile injection and a tornado missile height distribution. (orig.)

  2. Structural ballistic armour for transport aircraft

    OpenAIRE

    Horsfall, I; Austin, S J; Bishop, W.

    2000-01-01

    This paper describes the structural response of a current ceramic-faced composite armour system and a proposed structural armour system for aircraft use. The proposed structural ballistic armour system is shown to be capable of providing significant structural integrity even after ballistic impact whilst providing ballistic protection equivalent to an existing applique system. The addition of a carbon fibre reinforced plastic front panel to the existing ceramic faced composite armour system i...

  3. Earth--Mars Transfers with Ballistic Capture

    OpenAIRE

    Topputo, Francesco; Belbruno, Edward

    2014-01-01

    We construct a new type of transfer from the Earth to Mars, which ends in ballistic capture. This results in a substantial savings in capture $\\Delta v$ from that of a classical Hohmann transfer under certain conditions. This is accomplished by first becoming captured at Mars, very distant from the planet, and then from there, following a ballistic capture transfer to a desired altitude within a ballistic capture set. This is achieved by manipulating the stable sets, or sets of initial condit...

  4. Robust stability analysis for a cruise missile

    Institute of Scientific and Technical Information of China (English)

    Shi Yingjing; Ma Guangfu; Ma Hongzhong

    2008-01-01

    A global controller design methodology for a flight stage of the cruise missile is proposed.This methodology is based on the method of least squares.To prove robust stability in the full airspace with parameter disturbances.the Concepts of Convex polytopic models and quadratic stability are introduced.The effect of aerodynamic parameters on system performance is analyzed.The designed controller is applied to track the over loading signal of the cruise segment of the cruise missile,avoiding system disturbance owing to controller switching.Simulation results demonstrate the validity of the proposed method.

  5. The role of maxillofacial radiologists in gunshot injuries: a hypothesized missile trajectory in two case reports

    Science.gov (United States)

    Sansare, K; Khanna, V; Karjodkar, F

    2011-01-01

    Gunshot injuries are an emerging form of trauma that oral radiologists increasingly have to deal with. There are two main types of gunshot injuries: high-velocity and low-velocity bullet injuries. The outcome of high-velocity gunshot injury is usually fatal; however, a non-fatal low-velocity injury to the maxillofacial region is more likely to be encountered by the oral and maxillofacial radiologist. It is therefore important to up-to-date knowledge of ballistic science and its implications in the field of maxillofacial radiology. The ability of oral and maxillofacial radiologists to predict the missile trajectory will aid the assessment and localization of the damage caused by the bullet and its splinters. Predicting the missile trajectory may also be of help to law enforcement agencies and forensic scientists in determining the type of firearm used and direction of fire. This article, which examines two cases, attempts to highlight to the oral radiologist this emerging form of trauma and its implications. PMID:21159916

  6. CRANIOCEREBRAL MISSILE INJURY A STATISTICAL REVIEW

    Directory of Open Access Journals (Sweden)

    ALI ALIMOHAMMADI

    1986-05-01

    Full Text Available A Statistical report of 912 battle casualtiesadmitted in a special unit of the neurological surgery department during 49 months of the recent war was given. Methods of their evaluation, operative categories, management poli¬cies including techniques of Missile and bullet removal, and their complications were discussed.

  7. Minimum variation guidance laws for interceptor missiles

    NARCIS (Netherlands)

    Weiss, M.; Shima, T.

    2014-01-01

    This paper introduces a new approach to guidance law design using linear quadratic optimal control theory, minimizing throughout the engagement the variation of the control input as well as the integral control effort. The guidance law is derived for arbitrary order missile dynamics and target maneu

  8. Simulation missile trajectories generated by a tornado

    International Nuclear Information System (INIS)

    Revision 1 of Regulatory Guide 1.76, March 2007 establishes the criteria for evaluating nuclear plants against the adverse effects of a tornado. Basically, these effects can be summarized in three: effect of wind speed, effect of internal depression and effect of tornado-generated missiles tornado. The latter effect is to be considered in this paper.

  9. 77 FR 3514 - Protection Against Turbine Missiles

    Science.gov (United States)

    2012-01-24

    ... published in the Federal Register on November 2, 2009 (74 FR 56672) for a 60 day public comment period. DG-1217 was reissued for public comment on May 6, 2011 (76 FR 26320). The public comment period closed on... COMMISSION Protection Against Turbine Missiles AGENCY: Nuclear Regulatory Commission. ACTION:...

  10. Design and Implementation of Missile Guide Catalog%弹载导航星表的设计与实现

    Institute of Scientific and Technical Information of China (English)

    陆敬辉; 王宏力; 文涛; 陆长捷

    2011-01-01

    Based on the flight character of ballistic missile with short flight time and relatively steady flight attitude, a design method for the guide catalog of missile is proposed. The feature of projection of missile flight path is analyzed, which is a great circle in celestial sphere and an ellipse in XOY coordinate planes of the earth-centered inertial coordinate, and also the flight path is classified. Based on constraint conditions, the field of view ( FOV) of star sensor is determined, the stars in FOV are selected, and the guide catalog of missile is constructed and compared with traditional triangle catalog. The simulation shows that the method is simple, easy and small in storage capability. The problem which the right ascension is difficulty to express under tow-pole conditions is also is resolved by the method. In addition, the time for star map identification is reduced, the data output rate is enhanced, and the demand for application of stellar guidance placation to ballistic missile is satisfied.%根据弹道导弹飞行时间短,飞行姿态相对稳定的特性,提出了一种弹载导航星表的设计方法.分析了导弹飞行轨迹投影的特点,其在天球上投影为大圆,在地心惯性坐标系XOY平面上的投影为椭圆,并对飞行轨迹进行分类.根据限制条件,确定出星敏感器扫描的视场区域,挑选出视场中的恒星,构建出弹载导航星表,并与传统的三角形星表进行比较.仿真结果表明,该方法简单、易行,存储容量较小,同时避免了在两极的情况下,赤经难以表示的问题.减少了星图识别时间,提高了星光制导的数据输出率,满足了星光制导在弹道导弹上应用的要求.

  11. Rationale for wind-borne missile criteria for DOE facilities

    Energy Technology Data Exchange (ETDEWEB)

    McDonald, J R; Murray, R

    1999-09-01

    High winds tend to pick up and transport various objects and debris, which are referred to as wind-borne missiles or tornado missiles, depending on the type of storm. Missiles cause damage by perforating the building envelope or by collapsing structural elements such as walls, columns or frames. The primary objectives of this study are as follows: (1) to provide a basis for wind-borne or tornado missile criteria for the design and evaluation of DOE facilities, and (2) to provide guidelines for the design and evaluation of impact-resistant missile barriers for DOE facilities The first objective is accomplished through a synthesis of information from windstorm damage documentation experience and computer simulation of missile trajectories. The second objective is accomplished by reviewing the literature, which describes various missile impact tests, and by conducting a series of impact tests at a Texas Tech University facility to fill in missing information.

  12. Quantum Computation with Ballistic Electrons

    OpenAIRE

    Ionicioiu, Radu; Amaratunga, Gehan; Udrea, Florin

    2000-01-01

    We describe a solid state implementation of a quantum computer using ballistic single electrons as flying qubits in 1D nanowires. We show how to implement all the steps required for universal quantum computation: preparation of the initial state, measurement of the final state and a universal set of quantum gates. An important advantage of this model is the fact that we do not need ultrafast optoelectronics for gate operations. We use cold programming (or pre-programming), i.e., the gates are...

  13. Ballistic electron transport in mesoscopic samples

    International Nuclear Information System (INIS)

    In the framework of this thesis, the electron transport in the ballistic regime has been studied. Ballistic means that the lateral sample dimensions are smaller than the mean free path of the electrons, i.e. the electrons can travel through the whole device without being scattered. This leads to transport characteristics that differ significantly from the diffusive regime which is realised in most experiments. Making use of samples with high mean free path, features of ballistic transport have been observed on samples with sizes up to 100 μm. The basic device used in ballistic electron transport is the point contact, from which a collimated beam of ballistic electrons can be injected. Such point contacts were realised with focused ion beam (FIB) implantation and the collimating properties were analysed using a two opposite point contact configuration. The typical angular width at half maximum is around 50 , which is comparable with that of point contacts defined by other methods. (orig.)

  14. The nuclear-armed Tomahawk Cruise Missile: its potential utility on United States and United Kingdom attack submarines

    OpenAIRE

    Reynolds, Guy B.

    1998-01-01

    Approved for public release; distribution is unlimited. In July 1998, Britain published its Strategic Defense Review(SDR). The SDR outlined significant changes for Britain's nuclear weapons program and formalized the policy of sub-strategic deterrence using the Trident missile. It is unprecedented for a nuclear power to havec onsolidated its strategic and sub- strategic nuclear forces into a single system. The benefits offered by the British choice might be enjoyed for only a short time. T...

  15. THE EVIDENTIARY VALUE OF BALLISTIC EXPERTS

    OpenAIRE

    Shubhada Pednekar; B. Yuvakumar Reddy

    2015-01-01

    The science of ‘ballistics’ has been developed to facilitate the examination offirearms, ammunition and other related matter. But the terms ‘ballistics’is generally used to referto the study of the trajectory of bullets or missiles rather than of the missiles (bullets), and themiscible launchers (Guns) themselves. More appropriately the phrase ‘Forensic Ballistics’which was first coined by Colonel Goddard, a pioneer in this study, means the systematic studyof the firearms and ammunition used ...

  16. Reconnaissance radiological characterization for the White Point Nike Missile Site, San Pedro, California

    International Nuclear Information System (INIS)

    This report is the result of field work performed at the former White Point Nike Missile Site, San Pedro, California. The Hazardous Waste Remedial Actions Program tasked the Oak Ridge National Laboratory Pollutant Assessments Group in Grand Junction, Colo., with this project. The objective was to determine whether or not radioisotopes possibly associated with past Department of Defense (DOD) operations were present and within accepted background levels. The radiation survey was accomplished by performing three independent radiation surveys, both outdoors and indoors, and random soil sampling. Initially, the site was land surveyed to develop a grid block system. A background radiation investigation was performed out in the San Pedro area

  17. Ballistic and non-ballistic gas flow through ultrathin nanopores

    International Nuclear Information System (INIS)

    We show that ultrathin porous nanocrystalline silicon membranes exhibit gas permeance that is several orders of magnitude higher than other membranes. Using these membranes, gas flow obeying Knudsen diffusion has been studied in pores with lengths and diameters in the tens of nanometers regime. The components of the flow due to ballistic transport and transport after reflection from the pore walls were separated and quantified as a function of pore diameter. These results were obtained in pores made in silicon. We demonstrate that changing the pore interior to carbon leads to flow enhancement resulting from a change in the nature of molecule–pore wall interactions. This result confirms previously published flow enhancement results obtained in carbon nanotubes. (paper)

  18. A ballistics module as a part of the fire control system

    Directory of Open Access Journals (Sweden)

    Branka R. Luković

    2013-10-01

    Full Text Available This article presents a ballistics module as a part of the fire control system of weapons for fire support (mortars, artillery weapons and rocket launchers. The software is "open" with the prominence of autonomy work. It can be modulated and adapted on the user demand. Moreover, it is independent of the hardware base. Introduction: The fire control system is based on a ballistic module (BM which determines the firing data for each weapon tool in the battery. Ballistic calculations, for the given position of the target in relation to the position of tools in the given weather conditions, determine firing data (elevation, direction, timing and locating devices so that the missile seems to cause the desired effect. This paper gives the basic information about the features the BM performs and the manner of their implementation in the fire control system without going into algorithmic solution procedures. Ballistic problem in the fire control system: Ballistic calculation is based on a trajectory calculation of all kinds of projectiles (current, time-fuze, illuminating, smoke, with conventional propulsion, rocket, with built-in gas generator, etc.. Instead of previous solutions, where a trajectory calculation of the fire control system was done by approximate methods, in this BM the trajectory calculation is made by the same model with the same data as for a weapon and ammunition in the process of creating a firing table. The data used in the fire control system are made simultaneously with the preparation of firing tables for a particular tool and associated ammunition,. A modified model of particle, standardized at the NATO level, is also used. Taking into account the meteorological situation, before the trajectory calculation is done, a relative position of the target in relation to the position of the tool should be determined. A selection or loading check is carried out (possibility of reaching a given target as well as the point at which the

  19. Review on Empirical Studies of Local Impact Effects of Hard Missile on Concrete Structures

    Directory of Open Access Journals (Sweden)

    Ismail Abdul Rahman

    2011-05-01

    Full Text Available Concrete is basic construction material used for any kind of structure. However, in most vital and local structures such as nuclear plants, Power plants, Weapon Industries, weapons storage places, water retaining structures like dams, and also local industries, & etc., concrete structures have to be designed as defensive structures to provide protection against any accidents or knowingly generated incidents such as dynamic loading, dynamic local impact damage and global damage generated by kinetic missiles (steel rods, steel pipes, turbine blades, etc.. The impacting missile (projectile can be classified as ‘Hard’ and ‘Soft’ in nature, depending upon the implication of its deformation with respect to the deformation of target. ‘Hard’ missile impact can generate both local impact damage and also overall dynamic global damage of concrete structure. This paper only provides the review of previous empirical studies related to our study and can be used for making design recommendation and design procedures for determining the dynamic response of the target to prevent local and impact damage.

  20. Cooperative Guidance Law for Multiple Missiles With Terminal Impact Angle Constraint%带末端角度约束的多导弹协同制导律设计

    Institute of Scientific and Technical Information of China (English)

    惠耀洛; 南英; 陈哨东; 马晓华

    2015-01-01

    为了实现饱和攻击与饱和防御,提出了一种针对机动目标的多导弹协同制导律。建立了视线坐标系下的弹目相对运动数学模型,设计了三阶扩张状态观测器,对目标机动加速度项和运动方程中的耦合项进行观测与跟踪。在导弹飞行前段,基于滑模变结构理论设计了攻击时间可控的多导弹时间协同制导律;在导弹攻击末段,基于有限时间控制理论设计了满足终端角度约束的制导律,给出了导引律切换条件。仿真结果表明:该复合导引律能够使多枚导弹在满足攻击末端角度约束的条件下实现攻击时间协同;该制导律采用完备的空空导弹轨迹控制系统进行仿真,能够满足实际工程应用的要求。%A cooperative guidance law was proposed for multiple missiles in order to attack or defense against maneuvering targets at the same time.The equation of missile-target relative motion was established in sight line coordinate-system,and the third-order extended state observer was designed to observe and track acceleration of targets and coupling terms in the motion equation.The 4D impact-time control guidance law(ITCG)was designed in the forepart of interception based on the sliding mode control theory to ensure the attack time to be controlled.In the terminal ballistic traj ectory,another guidance law based on the finite time control theory was designed to meet the terminal angle constraint.Switching conditions of guidance law was also designed considering aspects of time and space.Numerical simulation results show that the attack time of multiple missiles is basically the same under the terminal attack angle constraint,and this guidance law can be used to combat maneuvering targets.The simulation is conducted using complete model of air-to-air missile,and this guidance law can be applied in actual proj ects.

  1. Computer Aided Aerodynamic Design of Missile Configuration

    OpenAIRE

    Panneerselvam, S; P. Theerthamalai; A.K. Sarkar

    1987-01-01

    Aerodynamic configurations of tactical missiles have to produce the required lateral force with minimum time lag to meet the required manoeuvability and response time. The present design which is mainly based on linearised potential flow involves (a) indentification of critical design points, (b) design of lifting components and their integration with mutual interference, (c) evaluation of aerodynamic characteristics, (d) checking its adequacy at otherpoints, (e) optimization of parameters an...

  2. On the Dynamic Stability of a Missile

    Directory of Open Access Journals (Sweden)

    K.C. Sharma

    1977-01-01

    Full Text Available The P-method given by Parks and Pritchard has been used to discuss the stability behaviour of a missile in free flight. General stability criteria for aerodynamic stabilisation have been obtained for slowly varying coefficients. The effect of pressure gradient on the stability of a coasting rocket has been explicitly examined. It is observed that the positive Magnus moment parameter ensures stability whereas a negative moment parameter would enhance the requirements of a larger stability margin.

  3. Impact load time histories for viscoelastic missiles

    International Nuclear Information System (INIS)

    Generation of the impact load time history at the contact point between a viscoelastic missile and its targets is presented. In the past, in the case of aircraft striking containment shell structure, the impact load time history was determined on the basis of actual measurements by subjecting a rigid wall to aircraft crash. The effects of elastic deformation of the target upon the impact load time history is formulated in this paper. The missile is idealized by a linear mass-spring-dashpot combination using viscoelastic models. These models can readily be processed taking into account the elastic as well as inelastic deformations of the missiles. The target is assumed to be either linearly elastic or rigid. In the case of the linearly elastic target, the normal mode theory is used to express the time-dependent displacements of the target which is simulated by lumped masses, elastic properties and dashpots in discrete parts. In the case of Maxwell viscoelastic model, the time-dependent displacements of the missile and the target are given in terms of the unknown impact load time history. This leads to an integral equation which may be solved by Laplace transformation. The normal mode theory is provided. The target structure may be composed of different materials with different components. Concrete and steel structural components have inherently different viscous friction damping properties. Hence, the equivalent modal damping depends on the degree of participation of these components in the modal response. An approximate rule for determining damping in any vibration mode by weighting the damping of each component according to the modal energy stored in each component is considered

  4. Modeling and Simulating Dynamics of Missiles with Deflectable Nose Control

    Institute of Scientific and Technical Information of China (English)

    Gao Yuan; Gu Liangxian; Pan Lei

    2009-01-01

    This article investigates the dynamic characteristics of deflectable nose missiles with rotary single-channel control. After introduction of effective attack and sideslip angles as well as quasi-body coordinates based on the spin characteristics of the missile's body, an integrated rigid kinetic model of missile with deflectable nose control is set up in the quasi-body coordinates considering the interaction between the missile's nose and body by using rootless multi-rigid-body system dynamics and is linearized. Then an analysis with simulation is conducted to investigate the coupling characteristics between the channels, the influences of nose deflection on the body and the dynamic characteristics of missile's body. The results indicate that various channels of missiles with deflectable nose control are coupled cross-linked; the nose deflection tends to make the body move in the opposite direction and, finally, evidences the correctness and reasonability of the kinetic model proposed by this article.

  5. Assessment of Ballistic Performance for Transparent Material

    Directory of Open Access Journals (Sweden)

    Basim M. Fadhil

    2014-05-01

    Full Text Available A finite element method was used to investigate the ballistic behavior of Polymethylmethacrylate (PMMA under impact loading by spherical steel projectile with different ranges of velocities. Three different target thicknesses were used in the experimental and the numerical works. A mathematical model has been used for the ballistic limit based on the experimental results. It has been found that projectile velocity and target thickness play an important role in the ballistic behavior of PMMA. A good agreement was found between the numerical, experimental, and the analytical result.

  6. Two distinct ballistic processes in graphene

    International Nuclear Information System (INIS)

    A dynamical approach to ballistic transport in mesoscopic graphene samples of finite length Land contact potential difference with leads U is developed. It is shown that at ballistic times shorter than both relevant time scales, tL = L/vg (vg - Fermi velocity) and tu = ħ/(eU), the major effect of electric field is to creates the electron - hole pairs, namely causes interband transitions. At ballistic times lager than the two scales the mechanism is very different. The conductivity has its “nonrelativistic” or intraband value equal to the one obtained within the Landauer-Butticker approach for the barrier Uresulting from evanescent waves tunneling through the barrier.

  7. Planetary Defense From Space: Part 1-Keplerian Theory

    Science.gov (United States)

    Maccone, Claudio

    A system of two space bases housing missiles is proposed to achieve the Planetary Defense of the Earth against dangerous asteroids and comets. We show that the layout of the Earth-Moon system with the five relevant Lagrangian (or libration) points in space leads naturally to only one, unmistakable location of these two space bases within the sphere of influence of the Earth. These locations are at the two Lagrangian points L1 (in between the Earth and the Moon) and L3 (in the direction opposite to the Moon from the Earth). We show that placing bases of missiles at L1 and L3 would cause those missiles to deflect the trajectory of asteroids by hitting them orthogonally to their impact trajectory toward the Earth, so as to maximize their deflection. We show that the confocal conics are the best class of trajectories fulfilling this orthogonal deflection requirement. An additional remark is that the theory developed in this paper is just a beginning of a larger set of future research work. In fact, while in this paper we only develop the Keplerian analytical theory of the Optimal Planetary Defense achievable from the Earth-Moon Lagrangian points L1 and L3, much more sophisticated analytical refinements would be needed to: Take into account many perturbation forces of all kinds acting on both the asteroids and missiles shot from L1 and L3; add more (non-optimal) trajectories of missiles shot from either the Lagrangian points L4 and L5 of the Earth-Moon system or from the surface of the Moon itself; encompass the full range of missiles currently available to the US (and possibly other countries) so as to really see "which asteroids could be diverted by which missiles", even in the very simplified scheme outlined here. Outlined for the first time in February 2002, our Confocal Planetary Defense concept is a Keplerian Theory that proved simple enough to catch the attention of scholars, representatives of the US Military and popular writers. These developments could

  8. Ballistic Fracturing of Carbon Nanotubes.

    Science.gov (United States)

    Ozden, Sehmus; Machado, Leonardo D; Tiwary, ChandraSekhar; Autreto, Pedro A S; Vajtai, Robert; Barrera, Enrique V; Galvao, Douglas S; Ajayan, Pulickel M

    2016-09-21

    Advanced materials with multifunctional capabilities and high resistance to hypervelocity impact are of great interest to the designers of aerospace structures. Carbon nanotubes (CNTs) with their lightweight and high strength properties are alternative to metals and/or metallic alloys conventionally used in aerospace applications. Here we report a detailed study on the ballistic fracturing of CNTs for different velocity ranges. Our results show that the highly energetic impacts cause bond breakage and carbon atom rehybridizations, and sometimes extensive structural reconstructions were also observed. Experimental observations show the formation of nanoribbons, nanodiamonds, and covalently interconnected nanostructures, depending on impact conditions. Fully atomistic reactive molecular dynamics simulations were also carried out in order to gain further insights into the mechanism behind the transformation of CNTs. The simulations show that the velocity and relative orientation of the multiple colliding nanotubes are critical to determine the impact outcome.

  9. UCAV path planning in the presence of radar-guided surface-to-air missile threats

    Science.gov (United States)

    Zeitz, Frederick H., III

    This dissertation addresses the problem of path planning for unmanned combat aerial vehicles (UCAVs) in the presence of radar-guided surface-to-air missiles (SAMs). The radars, collocated with SAM launch sites, operate within the structure of an Integrated Air Defense System (IADS) that permits communication and cooperation between individual radars. The problem is formulated in the framework of the interaction between three sub-systems: the aircraft, the IADS, and the missile. The main features of this integrated model are: The aircraft radar cross section (RCS) depends explicitly on both the aspect and bank angles; hence, the RCS and aircraft dynamics are coupled. The probabilistic nature of IADS tracking is accounted for; namely, the probability that the aircraft has been continuously tracked by the IADS depends on the aircraft RCS and range from the perspective of each radar within the IADS. Finally, the requirement to maintain tracking prior to missile launch and during missile flyout are also modeled. Based on this model, the problem of UCAV path planning is formulated as a minimax optimal control problem, with the aircraft bank angle serving as control. Necessary conditions of optimality for this minimax problem are derived. Based on these necessary conditions, properties of the optimal paths are derived. These properties are used to discretize the dynamic optimization problem into a finite-dimensional, nonlinear programming problem that can be solved numerically. Properties of the optimal paths are also used to initialize the numerical procedure. A homotopy method is proposed to solve the finite-dimensional, nonlinear programming problem, and a heuristic method is proposed to improve the discretization during the homotopy process. Based upon the properties of numerical solutions, a method is proposed for parameterizing and storing information for later recall in flight to permit rapid replanning in response to changing threats. Illustrative examples are

  10. Numerical investigation of missiles acceleration by hydrogen explosion

    International Nuclear Information System (INIS)

    Interaction of missile with the gas flow was studied numerically by means of three-dimensional gasdynamic computer code. Aerodynamic tube was modelled in which missiles of different shape were inserted in supersonic gas flow. Mach number and specific heat ratio of the flow as well as missile's orientation with respect to the flow were varied. Dependencies of drag coefficient of missiles on Mach number and specific heat ratio under conditions, that are typical to an accident in nuclear power plant, were evaluated. They are presented together with distributions of parameters of the gas flow around missile. It was shown that dependence of drag coefficient on specific heat ratio of the gas is not steep and may be omitted in evaluation of missile hazard. The method, which is used in evaluation of drag coefficients, is based on direct numerical simulation of hydrodynamics of the gaseous flow. It can be applied to obtain the exact values of drag coefficients under various conditions. Direct simulations of missile acceleration were performed under the following conditions. Compartment of 8 by 6 by 2.2 m size was filled with stoichiometric hydrogen-air mixture. Detonation was ignited at the centre of the shorter wall. Part of the opposite wall (2.2 by 1.2 m) could move freely under the pressure stress from detonation wave and form the missile. In five tests wall thickness, missile thickness and its mass were varied. Resulting missiles' velocities, distributions of gas flow parameters, and pressure loads are presented. Results of these numerical tests give the data on the missile velocities and momenta in some typical cases. Scaling relationships are proposed. The results of numerical tests and scaling relationships provide the estimation of velocities and momenta of missiles that are possible under accidental conditions. (J.P.N.)

  11. Design Philosophy of variable Mass Preformed Fragmented Missile Warhead

    OpenAIRE

    K.P.S. Murthy; K. Rama Rao; M.R. Patkar

    1992-01-01

    Fragment hit density and hit probability of the warhead are the critical parameters in the selection of a preformed fragment-type missile warhead against ground targets. Hence these factors are to be maximised. The parametric studies of these factors have lead to a new concept of variable mass preformed fragmented (VMPF) warhead. A philosophy was evolved for the VMPF-type missile warheads. A computer software for generating the external configuration of the VMPF-type missile warhead w...

  12. Missile autopilot design considering uncertainties in aerodynamics and actuator dynamics

    Science.gov (United States)

    Song, Yong D.; Hou, J.; Fogson, F.

    2000-07-01

    This work presents a method for missile autopilot design in the presence of actuator and uncertain dynamics. Nonlinear control algorithms are derived based on both missile aerodynamics and actuator dynamics. To account for system nonlinearities and uncertainties due to varying flight conditions, a memory-based compensation unit is developed and integrated into the strategy. Simulation on EMRAAT missile validates the effectiveness of the proposed control method.

  13. Reliability Simulation for a Missile Tank Under Random Loading

    Institute of Scientific and Technical Information of China (English)

    2001-01-01

    This paper presents a Monte-Carlo simulation method to calculate intensity relia- bility for a missile tank under random loading. The cumulative damage mathematical mod- el is established, and it adopts a direct simulation method to present random loading and o-riginal intensity for a missile tank. It can effectively predict intensity reliability for a missile tank in the environment of transport and flight.

  14. Influence of IR sensor technology on the military and civil defense

    Science.gov (United States)

    Becker, Latika

    2006-02-01

    Advances in basic infrared science and developments in pertinent technology applications have led to mature designs being incorporated in civil as well as military area defense systems. Military systems include both tactical and strategic, and civil area defense includes homeland security. Technical challenges arise in applying infrared sensor technology to detect and track targets for space and missile defense. Infrared sensors are valuable due to their passive capability, lower mass and power consumption, and their usefulness in all phases of missile defense engagements. Nanotechnology holds significant promise in the near future by offering unique material and physical properties to infrared components. This technology is rapidly developing. This presentation will review the current IR sensor technology, its applications, and future developments that will have an influence in military and civil defense applications.

  15. Intelligent Design and Implementation of Missile Fire Control System

    Institute of Scientific and Technical Information of China (English)

    XIE Chun-si; WANG Min-qing; LI Wei-hai; LIU Xi-zuo; JIN Liang-an

    2006-01-01

    Missile fire control system is the core of ship-based missile weapon system, whose safeguard levelhas direct relation with the attack ability of naval vessels. After a long period of deep investigation and research, it was found that, in one missile fire control system, there are such problems as single safeguard system, low ratio of cost to efficiency, etc. By adopting intelligent control techniques and many measures to multiple securities, the new type of assistant system is designed, some difficult problems are solved, such as fixed project channel and unitary means of missiles, which can make the equipment carry out combat mission reliably and continuously.

  16. Army hypersonic compact kinetic-energy missile laser window design

    Science.gov (United States)

    Russell, Gerald W.; Cayson, Stephen C.; Jones, Michael M.; Carriger, Wendy; Mitchell, Robert R.; Strobel, Forrest A.; Rembert, Michael; Gibson, David A.

    2003-09-01

    The U.S. Army Aviation and Missile Command, Aviation and Missile Research, Engineering, and Development Center (AMRDEC) is currently developing the Compact Kinetic Energy Missile (CKEM) which achieves hypersonic velocities at sea level. The system incorporates guidance to the target and requires active guidance technology. CKEM's kinetic energy warhead requires an accurate guidance sub-system in order to achieve high probability of kills at long range. Due to the severity of the aerothermal environments, minimized reaction time for small time to target conditions, and the communication degrading effects of the missile's energetic boost motor, a state of the art guidance technique is being developed by the AMRDEC Missile Guidance Directorate called Side-Scatter Laser Beam Rider. This technology incorporates a 1.06 micron laser to receive an off-axis laser guidance link to communicate guidance information from the launch site to the missile. This concept requires the use of optical windows on board the missile for the missile-borne laser energy signal receivers. The current concept utilizes four rectangular windows at 90° increments around the missile. The peak velocity during flight can reach approximately 6300 ft/sec inducing severe aerothermal heating and highly transient thermal gradients. The Propulsion and Structures Directorate was tasked to design and experimentally validate the laser window. Additionally, flight tests were conducted to demonstrate the laser guidance technology. This paper will present the laser window design development process as well as aerothermal testing to induce flight like environments and assess worst case thermostructural conditions.

  17. Ballistic Rail Gun Soft Recovery Facility

    Data.gov (United States)

    Federal Laboratory Consortium — The Ballistic Rail Gun Soft Recovery Facility accommodates a 155mm Howitzer, fired horizontally into a 104-foot long water trough to slow the projectile and recover...

  18. THEORETICAL DIFFRACTIVE FILTER PERFORMANCE FOR BALLISTIC TRANSILLUMINATION

    OpenAIRE

    Vacas-jacques, Paulino; Ryabukho, Vladimir; Strojnik, Marija; Tuchin, Valery; Paez, Gonzalo

    2009-01-01

    We address the topic of selectively probing turbid media, equivalent to biological tissue, with ballistic photons. The samples considered exhibit highly forward-directed scattering (anisotropy factor g > 0.9). We propose the utilization of a non-linear grating-based angular filter to separate the faint ballistic signal from optical noise. The filter is conformed of a monochromatic source incident on a ruled grating, positioned at grazing diffraction, followed by a narrow slit. Minute devia...

  19. IR sensor design insight from missile-plume prediction models

    Science.gov (United States)

    Rapanotti, John L.; Gilbert, Bruno; Richer, Guy; Stowe, Robert

    2002-08-01

    Modern anti-tank missiles and the requirement of rapid deployment have significantly reduced the use of passive armour in protecting land vehicles. Vehicle survivability is becoming more dependent on sensors, computers and countermeasures to detect and avoid threats. An analysis of missile propellants suggests that missile detection based on plume characteristics alone may be more difficult than anticipated. Currently, the passive detection of missiles depends on signatures with a significant ultraviolet component. This approach is effective in detecting anti-aircraft missiles that rely on powerful motors to pursue high-speed aircraft. The high temperature exhaust from these missiles contains significant levels of carbon dioxide, water and, often, metal oxides such as alumina. The plumes emits strongest in the infrared, 1 to 5micrometers , regions with a significant component of the signature extending into the ultraviolet domain. Many anti-tank missiles do not need the same level of propulsion and radiate significantly less. These low velocity missiles, relying on the destructive force of shaped-charge warhead, are more difficult to detect. There is virtually no ultraviolet component and detection based on UV sensors is impractical. The transition in missile detection from UV to IR is reasonable, based on trends in imaging technology, but from the analysis presented in this paper even IR imagers may have difficulty in detecting missile plumes. This suggests that the emphasis should be placed in the detection of the missile hard body in the longer wavelengths of 8 to 12micrometers . The analysis described in this paper is based on solution of the governing equations of plume physics and chemistry. These models will be used to develop better sensors and threat detection algorithms.

  20. Projectile penetration into ballistic gelatin.

    Science.gov (United States)

    Swain, M V; Kieser, D C; Shah, S; Kieser, J A

    2014-01-01

    Ballistic gelatin is frequently used as a model for soft biological tissues that experience projectile impact. In this paper we investigate the response of a number of gelatin materials to the penetration of spherical steel projectiles (7 to 11mm diameter) with a range of lower impacting velocities (number of predictive relationships available in the literature, it is found that over the range of projectiles and compositions used, the results fit a simple relationship that takes into account the projectile diameter, the threshold velocity for penetration into the gelatin and a value of the shear modulus of the gelatin estimated from the threshold velocity for penetration. The normalised depth is found to fit the elastic Froude number when this is modified to allow for a threshold impact velocity. The normalised penetration data are found to best fit this modified elastic Froude number with a slope of 1/2 instead of 1/3 as suggested by Akers and Belmonte (2006). Possible explanations for this difference are discussed. PMID:24184862

  1. REVOLUTION IN MILITARY AFFAIRS, MISSILE DEFENCE AND WEAPONS IN SPACE: THE US STRATEGIC TRIAD

    Directory of Open Access Journals (Sweden)

    Joelien Pretorius

    2011-07-01

    Full Text Available American plans for Missile Defence (MD and the weaponisation of space should be analysed in the larger framework of the contemporary Revolution in Military Affairs (RMA.1 Soviet military analysts have written about this revolution from as early as the 1970s, but it was the application of information age technology (IT in the 1991 Gulf War that captured the imagination of military planners and policy makers, especially in the US. The US is actively pursuing an RMA, conceptualised as integrating new IT into weapons systems and integrated command, control, computers, intelligence, surveillance and reconnaissance (C4ISR and, in turn, doctrinal, operational and organisational change in the military to take advantage of information dominance on the battlefield. This relates to MD and the weaponisation of space in two ways. Firstly, very few countries have the financial and technological capability to modernise their defence forces along the lines of a US-defined RMA, which means that they may resort to so-called asymmetric means to exploit the vulnerabilities or weaknesses of a strong, conventional power. Ballistic missiles (in association with chemical, biological or nuclear payloads are one of the asymmetrical threats most commonly cited in speeches and military documents of the US and used as justification of MD. Secondly, the RMA increases the US military’s reliance on space-based military assets for C4ISR. Placing weapons in space to protect these assets is seen as a logical step to ensure a key aspect of US dominance on the battlefield. This paper

  2. 用战术激光武器反巡航导弹%Using Tactical Laser Weapon to Hit Cruise Missile

    Institute of Scientific and Technical Information of China (English)

    刘淑英; 邵元培; 等

    2001-01-01

    This paper briefly describes the importance of hitting cruise missile in the modern war. According to the features of laser weapon tactical laser weapons are best suitable to intercept cruise missile and become one of important weapons to attack cruise missile. The paper also describes the researches and applications of tactical air defense laser weapons abroad. Finally the fundamental situation of tactical air defense laser weapons to hit cruise missile are dissussed.%简要说明了现代战争中反巡航导弹空袭的重要性,并从激光武器的特点出发说明战术防空激光武器是最适宜于用来反巡航导弹的武器,将成为反巡航导弹的重要武器之一。简要讲述了国外战术防空激光武器的研制情况及将其用于反巡航导弹的一些研究工作。最后论述了反巡航导弹的战术防空激光武器的基本状况。

  3. CT analysis of missile head injury

    International Nuclear Information System (INIS)

    Between August 1991 and December 1992, CT was performed in 154 patients who had suffered missile head injury during the war in the Republic of Croatia. In 54% CT was performed 1-24 h after injury, and in 27% follow-up CT was also obtained. The wounds were penetrating, tangential or perforating (45%, 34% and 21%, respectively). Haemorrhage was the most frequent lesion in the brain (84%). Follow-up CT evolution of haemorrhage, oedema, cerebritis, abscess, secondary vascular lesions, necrosis, encephalomalacia and hydrocephalus. The most dynamic changes occurred 7-14 days after injury. In 14% of cases, deep cerebral lesions were found in the corpus callosum, septum pellucidum periventricular region and pons, although bone and shell fragments were in a different part of the brain parenchyma. Such lesions were found in penetrating injuries only. CT proved very useful for assessing the extent and type of lesions. Although different mechanisms of brain damage in missile head injury are known, here they are, to the best of our knowledge, shown for the first time by CT. (orig.)

  4. Recent Advances in Antitank Guided Missile Systems

    Directory of Open Access Journals (Sweden)

    N. R. Iyer

    1995-07-01

    Full Text Available The recent advances in tactical antitank guided missile (ATGM systems are discussed. The main driving factors for the technological advances towards realisation of third generation ATGM systems have been the more demanding operational needs of the user services and limitations of earlier generation ATGM systems. The tasks of system design, hardware realisation, integration, testing and qualification have become extremely challenging to meet these stringent operational requirements. The technologies required to be mobilised for meeting these operational requirements and performance envelope and satisfying the operational and logistics constraints are again very demanding. The high technology content and the high level of performance required out of the subsystems have led to the present generation missile systems. The evolution from the earlier generations to current systems has been briefly discussed. Imaging infrared (IIR and Millimetre wave (MMW guidance systems employed for achieving the fire and forget capability of the third generation ATGM are described with specific reference to progress achieved so far. Translating the mission requirements to preliminary system specifications is another area wherein an innovative approach only can lead to meet the multiple performance criteria. Performance growth profile and emerging trends in ATGM systems are also analysed.

  5. Modern control theory for Army missile guidance

    Science.gov (United States)

    Travassos, R. H.; Levari, H.; Gupta, N. K.

    1982-11-01

    A Singular perturbation guidance law has been developed for medium-range surface-to-air missiles. This guidance law is a significant extension of a previously developed guidance law for short-range missiles; in medium-range intercepts, the problem of energy management should be addressed in addition to homing guidance. The mathematical formulation has been simplified by introducing separation of time scales. Target Trajectory Estimation: A recursive algorithm for estimation of autoregressive moving average (ARMA) model parameters from noisy samples has been developed. Application of this algorithm to parameter estimation problems has exhibited its fast convergence and unbiasedness in the presence of noise, even with short data records. The algorithm has two versions, a Recursive Maximum Likelihood (RML) form and a Recursive Prediction Error (RPE) form, both of which possess a parallel structure that makes them highly suitable for parallel-processing implementation. Adaptive autopilots: Lattice-form algorithms have been developed for fast, recursive identification and control of time-varying systems. These algorithms have excellent numerical properties and a modular structure that makes them suitable for on-board real-time implementation.

  6. CT analysis of missile head injury

    Energy Technology Data Exchange (ETDEWEB)

    Besenski, N. [Dept. of Radiology, Zagreb Univ. Hospital Rebro (Croatia); Jadro-Santel, D. [Dept. of Neuropathology, Zagreb Univ. Hospital Rebro (Croatia); Jelavic-Koic, F. [Dept. of Radiology, General Hospital Sveti Duh, Zagreb (Croatia); Pavic, D. [Dept. of Neuropathology, Zagreb Univ. Hospital Rebro (Croatia); Mikulic, D. [Zagreb School of Medicine (Croatia); Glavina, K. [Dept. of Radiology, Clinical Hospital, Osijek (Croatia); Maskovic, J. [Dept. of Radiology, Clinical Hospital, Split (Croatia)

    1995-04-01

    Between August 1991 and December 1992, CT was performed in 154 patients who had suffered missile head injury during the war in the Republic of Croatia. In 54% CT was performed 1-24 h after injury, and in 27% follow-up CT was also obtained. The wounds were penetrating, tangential or perforating (45%, 34% and 21%, respectively). Haemorrhage was the most frequent lesion in the brain (84%). Follow-up CT evolution of haemorrhage, oedema, cerebritis, abscess, secondary vascular lesions, necrosis, encephalomalacia and hydrocephalus. The most dynamic changes occurred 7-14 days after injury. In 14% of cases, deep cerebral lesions were found in the corpus callosum, septum pellucidum periventricular region and pons, although bone and shell fragments were in a different part of the brain parenchyma. Such lesions were found in penetrating injuries only. CT proved very useful for assessing the extent and type of lesions. Although different mechanisms of brain damage in missile head injury are known, here they are, to the best of our knowledge, shown for the first time by CT. (orig.)

  7. Ballistic self-annealing during ion implantation

    International Nuclear Information System (INIS)

    Ion implantation conditions are considered during which the energy, dissipated in the collision cascades, is low enough to ensure that the defects, which are generated during these collisions, consist primarily of vacancies and interstitial atoms. It is proposed that ballistic self-annealing is possible when the point defect density becomes high enough, provided that none, or very few, of the interstitial atoms escape from the layer being implanted. Under these conditions, the fraction of ballistic atoms, generated within the collision cascades from substitutional sites, decreases with increasing ion dose. Furthermore, the fraction of ballistic atoms, which finally end up within vacancies, increases with increasing vacancy density. Provided the crystal structure does not collapse, a damage threshold should be approached where just as many atoms are knocked out of substitutional sites as the number of ballistic atoms that fall back into vacancies. Under these conditions, the average point defect density should approach saturation. This model is applied to recently published Raman data that have been measured on a 3 MeV He+-ion implanted diamond (Orwa et al 2000 Phys. Rev. B 62 5461). The conclusion is reached that this ballistic self-annealing model describes the latter data better than a model in which it is assumed that the saturation in radiation damage is caused by amorphization of the implanted layer. (author)

  8. Novel micro-doppler signature extraction method of ballistic midcourse target%弹道目标进动周期特征提取新方法

    Institute of Scientific and Technical Information of China (English)

    雷腾; 刘进忙; 李松; 胡国平

    2013-01-01

    中段弹道目标识别一直是反导作战中的技术难点,而弹道目标微动产生的微多普勒信号为雷达识别弹头和诱饵提供了一种新的途径.针对弹道目标的进动特性,建立了锥体弹头的进动微多普勒模型,引入了时频重排平滑伪Wigner-Ville分布(RSPWVD)对锥体弹头的微多普勒信号进行了提取,仿真比较了Wigner-Ville分布(WVD)、平滑伪Wigner-Ville分布(SPWVD)和RSPWVD的提取结果,证明了RSPWVD在提取弹道目标微多普勒信号中的优越性,提出了一种基于微多普勒时频图的弹道目标进动周期特征提取新方法.仿真结果表明该方法具有很好的估计精度和抗噪性.%The identification of ballistic midcourse targets is always the difficult point in anti-missile system, while a new approach to identify the warhead is provided by the micro-Doppler of ballistic target. According to the characteristics of precession ballistic targets, the mathematical model of pyramidal ballistic missile warhead is established. Applying RSPWVD time-frequency transform to extracting the micro-Doppler signal, RSPWVD is seen as the best compared with WVD and SPWVD through simulation figures. Furthermore, an innovative method based on micro-Doppler time-frequency image to extract precession period is proposed. The results of simulation suggest that the innovative method has high precision and good performance of anti-noise.

  9. Modeling terminal ballistics using blending-type spline surfaces

    Science.gov (United States)

    Pedersen, Aleksander; Bratlie, Jostein; Dalmo, Rune

    2014-12-01

    We explore using GERBS, a blending-type spline construction, to represent deform able thin-plates and model terminal ballistics. Strategies to construct geometry for different scenarios of terminal ballistics are proposed.

  10. Misleading reference to unpublished wound ballistics data regarding distant injuries

    OpenAIRE

    Courtney, Michael; Courtney, Amy

    2008-01-01

    An article (J Trauma 29:10-18, 1989) cites unpublished wound ballistics data to support the authors' view that distant injuries are a myth in wound ballistics. The actual data, published in 1990, actually contains a number of detailed examples of distant injuries. (Bellamy RF, Zajtchuk R. The physics and biophysics of wound ballistics. In: Zajtchuk R, ed. Textbook of Military Medicine, Part I: Warfare, Weaponry, and the Casualty, Vol. 5, Conventional Warfare: Ballistic, Blast, and Burn Injuri...

  11. Earth--Mars Transfers with Ballistic Capture

    CERN Document Server

    Topputo, Francesco

    2014-01-01

    We construct a new type of transfer from the Earth to Mars, which ends in ballistic capture. This results in a substantial savings in capture $\\Delta v$ from that of a classical Hohmann transfer under certain conditions. This is accomplished by first becoming captured at Mars, very distant from the planet, and then from there, following a ballistic capture transfer to a desired altitude within a ballistic capture set. This is achieved by manipulating the stable sets, or sets of initial conditions whose orbits satisfy a simple definition of stability. This transfer type may be of interest for Mars missions because of lower capture $\\Delta v$, moderate flight time, and flexibility of launch period from the Earth.

  12. Ballistic Response of Fabrics: Model and Experiments

    Science.gov (United States)

    Orphal, Dennis L.; Walker Anderson, James D., Jr.

    2001-06-01

    Walker (1999)developed an analytical model for the dynamic response of fabrics to ballistic impact. From this model the force, F, applied to the projectile by the fabric is derived to be F = 8/9 (ET*)h^3/R^2, where E is the Young's modulus of the fabric, T* is the "effective thickness" of the fabric and equal to the ratio of the areal density of the fabric to the fiber density, h is the displacement of the fabric on the axis of impact and R is the radius of the fabric deformation or "bulge". Ballistic tests against Zylon^TM fabric have been performed to measure h and R as a function of time. The results of these experiments are presented and analyzed in the context of the Walker model. Walker (1999), Proceedings of the 18th International Symposium on Ballistics, pp. 1231.

  13. Innovation in Aerodynamic Design Features of Soviet Missiles

    Science.gov (United States)

    Spearman, M. Leroy

    2006-01-01

    Wind tunnel investigations of some tactical and strategic missile systems developed by the former Soviet Union have been included in the basic missile research programs of the NACA/NASA. Studies of the Soviet missiles sometimes revealed innovative design features that resulted in unusual or unexpected aerodynamic characteristics. In some cases these characteristics have been such that the measured performance of the missile exceeds what might have been predicted. In other cases some unusual design features have been found that would alleviate what might otherwise have been a serious aerodynamic problem. In some designs, what has appeared to be a lack of refinement has proven to be a matter of expediency. It is a purpose of this paper to describe some examples of unusual design features of some Soviet missiles and to illustrate the effectiveness of the design features on the aerodynamic behavior of the missile. The paper draws on the experience of the author who for over 60 years was involved in the aerodynamic wind tunnel testing of aircraft and missiles with the NACA/NASA.

  14. Gauging the Influence of Technology on Tactical Missiles of the Future(Short Communication

    Directory of Open Access Journals (Sweden)

    Mark L. Bundy

    2002-01-01

    Full Text Available Tactical missiles, carrying kinetic energy, high explosives, or multiple submunitions are an integral part of the current and future US Army weapons inventory. Naturally, the number of missiles that can be stowed on any mobile launch platform depends on the size of the missile. Advances in rocket propulsion efficiency and improvements in guidance systems may make it possible to reduce missile size without a proportionate decrease in effectiveness. A primitive I-DOF computer model is used here to show how advances in missile technology might allow smaller missiles in the future to carry out the mission of today's larger missiles. A scaled-down version of a typical current generation missile is taken as the next generation missile. Hypothetical improvements in this smaller missile are then chosen in four basic areas-propellant impulse, burn time, weight fraction, and aerodynamic drag.-with the effects on lethality reported in a nondimensional format.

  15. Ballistic thermal rectification in nanoscale three-terminal junctions

    Science.gov (United States)

    Zhang, Lifa; Wang, Jian-Sheng; Li, Baowen

    2010-03-01

    We study ballistic thermal transport in three-terminal atomic nanojunctions by the nonequilibrium Green’s function method. We find that there is ballistic thermal rectification in asymmetric three-terminal structures because of the incoherent phonon scattering from the control terminal. With spin-phonon interaction, we also find the ballistic thermal rectification even in symmetric three-terminal paramagnetic structures.

  16. Visual Simulation of Missile Attacking Battleplane Based on Vega

    Directory of Open Access Journals (Sweden)

    Zhang Huibing

    2013-07-01

    Full Text Available A visual simulation system of fragment warhead missile attacking F-16C ''Falcon'' battleplane based on simulation and virtual reality technology is put forward. Firstly, the overall design of visual simulation of missile attacking F16 battleplane is implemented, and all functions of each module are demonstrated in detailed. Then 3D models in virtual battle field are optimized by level of detail, texture mapping, billboard and instance technology. Finally, Vega scene driving program is developed, and the implementation of special effect, view transform, preview and collision detect are emphasized. The result of simulation provides reference for damage assessment of missile attacking F16 battleplane.

  17. Dynamic Simulation for Missile Erection System

    Institute of Scientific and Technical Information of China (English)

    2007-01-01

    In order to study the dynamic characteristics of the missile erection system, it can be considered as a rigid-flexible coupling multi-body system. Firstly, the actual system is abstracted as an equal and simplified one and then the forces applied to it are analyzed. Secondly, the rigid-flexible coupling dynamic simulation for erection system is accomplished by use of the system simulation software, for example Pro/E, ADAMS, ANSYS, MATLAB/Simulink, etc. Finally, having the aid of simulation results, the kinetic and dynamic characteristics of the flexible bodies in erection system are analyzed.The simulation considering the erection system as a rigid-flexible coupling system can provide valuable results to the research of its kinetic, dynamic and vibrational characteristics.

  18. Optical Kalman filtering for missile guidance

    Science.gov (United States)

    Casasent, D.; Neuman, C. P.; Lycas, J.

    1984-01-01

    Optical systolic array processors constitute a powerful and general-purpose set of optical architectures with high computational rates. In this paper, Kalman filtering, a novel application for these architectures, is investigated. All required operations are detailed; their realization by optical and special-purpose analog electronics are specified; and the processing time of the system is quantified. The specific Kalman filter application chosen is for an air-to-air missile guidance controller. The architecture realized in this paper meets the design goal of a fully adaptive Kalman filter which processes a measurement every 1 msec. The vital issue of flow and pipelining of data and operations in a systolic array processor is addressed. The approach is sufficiently general and can be realized on an optical or digital systolic array processor.

  19. Sidewall reflections in streamlined missile radomes

    Science.gov (United States)

    Huddleston, G. K.; Crockett, M. P.

    Predicted and measured patterns are presented which serve as dramatic illustrations of the 'LLoyd's mirror' effect, in which direct and reflected waves generate interference in the form of unexpected peaks and nulls in radome-enclosed receiving antenna patterns. These effects are associated with a low-gain antenna which is offset from the centerline of a streamlined tangent ogive radome intended for high-speed missile applications. Since many other airborne radome applications require that more than one antenna be located inside a radome cavity, these data furnish insight into what may be expected for offset-antenna locations. The geometrical optics approximations used to obtain reflected wave contributions are noted to be exceptionally accurate foir the small antennas considered.

  20. Reinforced concrete behavior due to missile impact

    International Nuclear Information System (INIS)

    The assessment of the safety of nuclear reactors has necessitated the study of the effect of missiles on reinforced concrete containment structures. Two simple theoretical calculational methods have been developed to provide basic information. The first is based on a crude energy balance approach in which that part of the kinetic energy of the missile which is transferred into the containment structure, is absorbed only as bending strain energy. To determine the energy transferred into the structure it is assumed that during the loading the target does not respond. The energy input to the structure is thus equal to the kinetic energy it will possess immediately the impulse has been removed. The boundary of the responding zone is defined by the distance travelled by the shear stress wave during the time in which the impact force increases to the load at which the shear capacity reaches the ultimate shear resistance. The second method is based on the equation of motion for an equivalent one-degree-of-freedom system assuming that only the peak value of deflection is important and that damping can be ignored. The spring stiffness of the equivalent system has been based upon the stiffness of the actual disc configuration responding in the flexural mode only. The boundaries of the disc have been defined by using the elastic plate formulae and equating those positive and negative moments which will produce a specified yield line pattern which may be inferred from plastic plate formulae. The equation of motion is solved to indicate how the quantity of reinforcement included in the structure may modify the peak deflection. By limiting the ductility ratio of the reinforcement to some prescribed level it is possible to indicate the quantity of reinforcement w

  1. Antioxidative defense

    Directory of Open Access Journals (Sweden)

    Stevanović Jelka

    2011-01-01

    Full Text Available Free radicals occur constantly during metabolism and take part in numerous physiological processes, such as: intra-cellular and inter-cellular signalization, gene expression, removal of damaged or senescent cells, and control of the tone of blood vessels. However, there is an increased quantity of free radicals in situations of so-called oxidative stress, when they cause serious damage to cellular membranes (peroxidation of their lipids, damage of membrane proteins, and similar, to interior cellular protein molecules, as well as DNA molecules and carbohydrates. This is precisely why the organism has developed numerous mechanisms for removing free radicals and/or preventing their production. Some of these are enzyme-related and include superoxide-dismutase, catalase, glutathione-peroxidase, and others. Other, non-enzyme mechanisms, imply antioxidative activities of vitamins E and C, provitamin A, coenzyme Q, reduced glutation, and others. Since free radicals can leave the cell that has produced them and become dispersed throughout the body, in addition to antioxidative defense that functions within cellular structures, antioxidant extra-cellular defense has also been developed. This is comprised by: transferrin, lactoferrin, haptoglobin, hemopexin, ceruloplasmin, albumins, extra-cellular isoform SOD, extracellular glutathione-peroxidase, glucose, bilirubin, urates, and many other molecules.

  2. Internal ballistics of guns and rockets

    Directory of Open Access Journals (Sweden)

    Asim Ray

    1964-07-01

    Full Text Available An exact analytical solutions of the equations relating to the internals ballistics of guns and rockets in the non-isothermal model using tubular propellants which burns according to the pressure-index law has been obtained. An approximate solution to a pre-assigned level of accuracy has been presented.

  3. The Internal Ballistics of an Air Gun

    Science.gov (United States)

    Denny, Mark

    2011-01-01

    The internal ballistics of a firearm or artillery piece considers the pellet, bullet, or shell motion while it is still inside the barrel. In general, deriving the muzzle speed of a gunpowder firearm from first principles is difficult because powder combustion is fast and it very rapidly raises the temperature of gas (generated by gunpowder…

  4. Electron Interference in Ballistic Graphene Nanoconstrictions

    DEFF Research Database (Denmark)

    Baringhaus, Jens; Settnes, Mikkel; Aprojanz, Johannes;

    2016-01-01

    We realize nanometer size constrictions in ballistic graphene nanoribbons grown on sidewalls of SiC mesa structures. The high quality of our devices allows the observation of a number of electronic quantum interference phenomena. The transmissions of Fabry-Perot-like resonances are probed...

  5. The Ballistic Cart on an Incline Revisited.

    Science.gov (United States)

    Serway, Raymond A.; And Others

    1995-01-01

    Presents the theory behind the mechanics demonstration that involves projecting a ball vertically upward from a ballistic cart moving along an inclined plane. The measured overshoot is believed to be due, in part, to the presence of rolling friction and the inertial properties of the cart wheels. (JRH)

  6. The National Ballistics Imaging Comparison (NBIC) project.

    Science.gov (United States)

    Song, J; Vorburger, T V; Ballou, S; Thompson, R M; Yen, J; Renegar, T B; Zheng, A; Silver, R M; Ols, M

    2012-03-10

    In response to the guidelines issued by the American Society of Crime Laboratory Directors/Laboratory Accreditation Board (ASCLD/LAB-International) to establish traceability and quality assurance in U.S. crime laboratories, a NIST/ATF joint project entitled National Ballistics Imaging Comparison (NBIC) was initialized in 2008. The NBIC project aims to establish a National Traceability and Quality System for ballistics identifications in crime laboratories within the National Integrated Ballistics Information Network (NIBIN) of the U.S. NIST Standard Reference Material (SRM) 2460 bullets and 2461 cartridge cases are used as reference standards. 19 ballistics examiners from 13 U.S. crime laboratories participated in this project. They each performed 24 periodic image acquisitions and correlations of the SRM bullets and cartridge cases over the course of a year, but one examiner only participated in Phase 1 tests of SRM cartridge case. The correlation scores were collected by NIST for statistical analyses, from which control charts and control limits were developed for the proposed Quality System and for promoting future assessments and accreditations for firearm evidence in U.S. forensic laboratories in accordance with the ISO 17025 Standard. PMID:22014973

  7. Is there ballistic transport in metallic nano-objects? Ballistic versus diffusive contributions

    Energy Technology Data Exchange (ETDEWEB)

    Garcia, N [Laboratorio de Fisica de Sistemas Pequenos y NanotecnologIa, Consejo Superior de Investigaciones CientIficas (CSIC), Madrid 28006 (Spain); Bai Ming [Laboratorio de Fisica de Sistemas Pequenos y NanotecnologIa, Consejo Superior de Investigaciones CientIficas (CSIC), Madrid 28006 (Spain); Lu Yonghua [Laboratorio de Fisica de Sistemas Pequenos y NanotecnologIa, Consejo Superior de Investigaciones CientIficas (CSIC), Madrid 28006 (Spain); Munoz, M [Laboratorio de Fisica de Sistemas Pequenos y NanotecnologIa, Consejo Superior de Investigaciones CientIficas (CSIC), Madrid 28006 (Spain); Cheng Hao [Laboratorio de Fisica de Sistemas Pequenos y NanotecnologIa, Consejo Superior de Investigaciones CientIficas (CSIC), Madrid 28006 (Spain); Levanyuk, A P [Fisintec Innovacion Tecnologica, Miraflores 65, Alcobendas, Madrid 28100 (Spain)

    2007-01-10

    When discussing the resistance of an atomic-or nanometre-size contact we should consider both its ballistic and its diffusive contributions. But there is a contribution of the leads to the resistance of the contact as well. In this context, the geometry and the roughness of the surfaces limiting the system will contribute to the resistance, and these contributions should be added to the ideal ballistic resistance of the nanocontact. We have calculated, for metallic materials, the serial resistance of the leads arising from the roughness, and our calculations show that the ohmic resistance is as important as the ballistic resistance of the constriction. The classical resistance is a lower limit to the quantum resistance of the leads. Many examples of earlier experiments show that the mean free path of the transport electrons is of the order of the size of the contacts or the leads. This is not compatible with the idea of ballistic transport. This result may put in serious difficulties the current, existing interpretation of experimental data in metals where only small serial resistances compared with the ballistic component of the total resistance have been taken into account. The two-dimensional electron gas (2DEG) is also discussed and the serial corrections appear to be smaller than for metals. Experiments with these last systems are proposed that may reveal new interesting aspects in the physics of ballistic and diffusive transport.

  8. Is there ballistic transport in metallic nano-objects? Ballistic versus diffusive contributions

    International Nuclear Information System (INIS)

    When discussing the resistance of an atomic-or nanometre-size contact we should consider both its ballistic and its diffusive contributions. But there is a contribution of the leads to the resistance of the contact as well. In this context, the geometry and the roughness of the surfaces limiting the system will contribute to the resistance, and these contributions should be added to the ideal ballistic resistance of the nanocontact. We have calculated, for metallic materials, the serial resistance of the leads arising from the roughness, and our calculations show that the ohmic resistance is as important as the ballistic resistance of the constriction. The classical resistance is a lower limit to the quantum resistance of the leads. Many examples of earlier experiments show that the mean free path of the transport electrons is of the order of the size of the contacts or the leads. This is not compatible with the idea of ballistic transport. This result may put in serious difficulties the current, existing interpretation of experimental data in metals where only small serial resistances compared with the ballistic component of the total resistance have been taken into account. The two-dimensional electron gas (2DEG) is also discussed and the serial corrections appear to be smaller than for metals. Experiments with these last systems are proposed that may reveal new interesting aspects in the physics of ballistic and diffusive transport

  9. Analysis and improvement of missile three-loop autopilots

    Institute of Scientific and Technical Information of China (English)

    Lin Defu; Fan Junfang; Qi Zaikang; Mou Yu

    2009-01-01

    characteristics from a two-loop autopilot with PI compensator.Both the two-loop and three-loop topologies can stabilize a static unstable missile.However,the finite actuator resource is the crucial factor dominating autopilot function.

  10. The Study of Tactical Missile's Airframe Digital Optimization Design

    Institute of Scientific and Technical Information of China (English)

    LUO Zhiqing; QIAN Airong; LI Xuefeng; GAO Lin; LEI Jian

    2006-01-01

    Digital design and optimal are very important in modern design. The traditional design methods and procedure are not fit for the modern missile weapons research and development. Digital design methods and optimal ideas were employed to deal with this problem. The disadvantages of the traditional missile's airframe design procedure and the advantages of the digital design methods were discussed. A new concept of design process reengineering (DPR) was put forward. An integrated missile airframe digital design platform and the digital design procedure, which integrated the optimization ideas and methods, were developed. Case study showed that the design platform and the design procedure could improve the efficiency and quality of missile's airframe design, and get the more reasonable and optimal results.

  11. Analysis of Nonlinear Missile Guidance Systems Through Linear Adjoint Method

    Directory of Open Access Journals (Sweden)

    Khaled Gamal Eltohamy

    2015-12-01

    Full Text Available In this paper, a linear simulation algorithm, the adjoint method, is modified and employed as an efficient tool for analyzing the contributions of system parameters to the miss - distance of a nonlinear time-varying missile guidance system model. As an example for the application of the linear adjoint method, the effect of missile flight time on the miss - distance is studied. Since the missile model is highly nonlinear and a time-varying linearized model is required to apply the adjoint method, a new technique that utilizes the time-reversed linearized coefficients of the missile as a replacement for the time-varying describing functions is applied and proven to be successful. It is found that, when compared with Monte Carlo generated results, simulation results of this linear adjoint technique provide acceptable accuracy and can be produced with much less effort.

  12. Design formula of reinforced concrete structures against rigid missile impact

    Energy Technology Data Exchange (ETDEWEB)

    Ito, Chihiro; Shirai, Koji; Ohnuma, Hiroshi [Central Research Inst. of Electric Power Industry, Abiko, Chiba (Japan). Abiko Research Lab.

    1995-01-01

    For the design of concrete containment structures built in nuclear power stations in Japan, internal pressure, temperature load and earthquake load have so far been considered as the major types of load that could result from accident. In some foreign countries, impact load caused by collision of missile is taken into consideration for the design of this kind of structures as well. Also in Japan, in the design of the repossessing plants which is now under construction at Shimokita area, air craft crash is taken into account. In this study, in order to establish the design method of concrete structures against impact due to collision of missile, the impact tests have been carried out using hard missile with the velocity from 4.0m/s to 250m/s. Based on these results, we proposed the design method of reinforced concrete structure against the collision of hard missile. (author).

  13. Research on Optimization Strategy of Missile Preliminary Design

    Institute of Scientific and Technical Information of China (English)

    SUZi-jian; ZHONGYi-fang

    2004-01-01

    Two system optimization architectures are proposed for missile system preliminary design, taking into account aerodynamics, weights and sizing, propulsion and trajectory.Approximation methods are investigated in order to reduce problem dimensionality and to improve the efficiency of optimization process.

  14. Density Models for Velocity Analysis of Jet Impinged CEDM Missile

    Energy Technology Data Exchange (ETDEWEB)

    Jo, Won Ho; Kang, Tae Kyo; Cho, Yeon Ho; Chang, Sang Gyoon; Lee, Dae Hee [KEPCO EnC, Daejeon (Korea, Republic of)

    2015-05-15

    A control element drive mechanism (CEDM) can be a potential missile in the reactor head area during one of the postulated accidents. The CEDM is propelled by the high speed water jet discharged from a broken upper head nozzle. The jet expansion models to predict the missile velocity have been investigated by Kang et al. The previous work of Kang et al. showed a continuous increase in missile velocity as the CEDM missile travels. But it is not natural in that two phase flow from the nozzle break exit tends to disperse and the thrust force on the missile decreases along the distance of the travel. The jet flow also interacts with the air surrounding itself. Therefore, the density change has to be included in the estimation of the missile velocity. In this paper, two density change models of the water jet are introduced for the jet expansion models along with the distance from the nozzle break location. The first one is the direct approximation model. Two density approximation models are introduced to predict the CEDM missile velocity. For each model, the effects of the expanded jet area were included as the area ratio to the exit nozzle area. In direct approximation model, the results have showed rapid decrease in both density and missile velocity. In pressure approach model, the density change is assumed perfectly proportional to the pressure change, and the results showed relatively smooth change in both density and missile velocity comparing to the direct approximation model. Using the model developed by Kang et al.., the maximum missile velocity is about 4 times greater comparing to the pressure approach model since the density is constant as the jet density at the nozzle exit in their model. Pressure approach model has benefits in that this model adopted neither curve fitting nor extrapolation unlike the direct approximation model, and included the effects of density change which are not considered in the model developed by Kang et al. So, this model is

  15. Application of Computer Graphics to Performance Studies of Missile Warheads

    OpenAIRE

    K. Rama Rao; K.P.S. Murthy; M.R. Patkar

    1991-01-01

    Intercept geometry of target aircraft and missiles play an important role in determining the effectiveness of the warhead. Factors such as fragment spatial distribution profile, damage capabilities, target and missile characteristics have been considered and visualised through computer graphics and optimum intercept intercept angles have been arrived. Computer graphics has proved to be an important tool to enhance perception and conceptual design capabilities in the design environment.

  16. Design and development of Propulsion System for Antitank Guided Missile

    OpenAIRE

    T. Mohan Reddy; A. Subanandha Rao; Sambasiva Rao, M.

    1995-01-01

    A Propulsion system is designed and developed for the third generation antitank guided missile (ATGM). It consists of a separate booster and sustainer. Booster is ahead of sustainer, having four nozzles canted to the missile axis. Sustainer discharges through a supersonic blast tube. Low smoke, high energy nitramine propellant for this propulsion system developed by the High Energy Materials Research Laboratory (HEMRL), Pune, has been successfully flight-tested. The booster grain is tu...

  17. Application of Computer Graphics to Performance Studies of Missile Warheads

    Directory of Open Access Journals (Sweden)

    K. Rama Rao

    1991-01-01

    Full Text Available Intercept geometry of target aircraft and missiles play an important role in determining the effectiveness of the warhead. Factors such as fragment spatial distribution profile, damage capabilities, target and missile characteristics have been considered and visualised through computer graphics and optimum intercept intercept angles have been arrived. Computer graphics has proved to be an important tool to enhance perception and conceptual design capabilities in the design environment.

  18. Changing law of launching pitching angular velocity of rotating missile

    OpenAIRE

    Liu Guang; Xu Bin; Jiao Xiaojuan; Zhen Tiesheng

    2014-01-01

    In order to provide accurate launching pitching angular velocity (LPAV) for the exterior trajectory optimization design, multi-flexible body dynamics (MFBD) technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model. The built model i...

  19. Active and Passive Precautions in Air and Missile Warfare

    OpenAIRE

    Sassoli, Marco; Quintin, Anne

    2014-01-01

    Based upon state practice, customary international law, Protocol Additional I to the Geneva Conventions and the Harvard Manual on Air and Missile Warfare (which they critically review), the authors discuss the different precautionary measures for the benefit of the civilian population an attacker and a defender must take, in the conduct of hostilities in general, and specifically in air and missile warfare, including in attacks against aircraft.

  20. Shipborne Laser Beam Weapon System for Defence against Cruise Missiles

    OpenAIRE

    J.P. Dudeja; G.S. Kalsey

    2000-01-01

    Sea-skim~ing cruise missiles pose the greatest threat to a surface ship in the present-day war scenario. The convenitional close-in-weapon-systems (CIWSs) are becoming less reliable against these new challenges requiring extremely fast reaction time. Naval Forces see a high energy laser as a feasible andjeffective directed energy weapon against sea-skimming antiship cruise missiles becauseof its .ability to deliver destructive energy at the speed of light on to a distant target. The paper com...

  1. Aerodynamics of powered missile separation from F/A-18 aircraft

    Science.gov (United States)

    Ahmad, J. U.; Shanks, S. P.; Buning, P. G.

    1993-01-01

    A 3D dynamic 'chimera' algorithm that solves the thin-layer Navier-Stokes equations over multiple moving bodies was modified to numerically simulate the aerodynamics, missile dynamics, and missile plume interactions of a missile separating from a generic wing and from an F/A-18 aircraft in transonic flow. The missile is mounted below the wing for missile separation from the wing and on the F/A-18 fuselage at the engine inlet side for missile separation from aircraft. Static and powered missile separation cases are considered to examine the influence of the missile and plume on the wing and F/A-18 fuselage and engine inlet. The aircraft and missile are at two degrees angle of attack, Reynolds number of 10 million, freestream Mach number of 1.05 and plume Mach number of 3.0. The computational results show the details of the flow field.

  2. MARVEL revisited: experiment design and data analysis. [In-trench environment of the MX missile system

    Energy Technology Data Exchange (ETDEWEB)

    Thomsen, J.M.

    1978-02-28

    As part of the research performed for the Defense Nuclear Agency program defining the in-trench environment for the MX missile system, the nuclear data base was reviewed to determine if any of it was applicable to the problem of air-shock attenuations in long, shallowly-buried tubes. Because of its unique shock-tube geometry, the LLL MARVEL event, fired in 1967, was judged one of the few relevant nuclear events. The MARVEL event is described, including emplacement geometry and emplacement of instrumentation to measure shock time-of-arrival (TOA) in the shock tube. TOA data from the event, including uncertainties, are discussed and analyzed. Finally, using shock-tube theory, the flow parameters D (shock-tube velocity) and P (peak pressure in the air behind the shock front) are derived from a fit to the MARVEL TOA data. The data derived from those parameters are consistent.

  3. Considerations of a ship defense with a pulsed COIL

    Science.gov (United States)

    Takehisa, K.

    2015-10-01

    Ship defense system with a pulsed COIL (Chemical Oxygen-Iodine Laser) has been considered. One of the greatest threats for battle ships and carriers in warfare are supersonic anti-ship cruise missiles (ASCMs). A countermeasure is considered to be a supersonic RAM (Rolling Airframe Missile) at first. A gun-type CIWS (Close-In Weapon System) should be used as the last line of defense. However since an ASCM can be detected at only 30-50km away due to radar horizon, a speed-of-light weapon is desirable as the first defense especially if the ASCM flies at >Mach 6. Our previous report explained several advantages of a giant pulse from a chemical oxygen laser (COL) to shoot down supersonic aircrafts. Since the first defense has the target distance of ~30km, the use of COIL is better considering its beam having high transmissivity in air. Therefore efficient operation of a giant-pulsed COIL has been investigated with rate-equation simulations. The simulation results indicate that efficient single-pass amplification can be expected. Also a design example of a giant-pulsed COIL MOPA (master oscillator and power amplifier) system has been shown, in which the output energy can be increased without limit.

  4. China's nuclear arsenal and missile defence

    International Nuclear Information System (INIS)

    Over the last few years, major focus of the nuclear debate has been turned towards the United States' proposal to erect a National Missile Defence (NMD) shield for itself. Of the existing nuclear weapon powers, China has been the most vociferous critic of this proposal. As and when this shield does become a reality, China will be the first to lose credibility as a deterrent against USA's existing nuclear arsenal. Therefore taking countermeasures against such a proposal is quite natural. China's approach towards non-proliferation mechanisms is steeped in realpolitik and its ability to manoeuvre them in its favour as a P5 and N5 power. Further, the Chinese leadership have been clear about the capabilities and limitations of nuclear weapons and treated them as diplomatic and political tools. The underlying aim is to preserve China's status as a dominant player in the international system while checkmating other possible challengers. Such a pragmatic approach is of far-reaching significance to all nations, especially those that possess nuclear weapons themselves. It will also be in India's long-term strategic interest to assess and take necessary corrective measures in its national security strategy, and make the composition of Indian nuclear strategy meet the desired goal. (author)

  5. Computer Aided Aerodynamic Design of Missile Configuration

    Directory of Open Access Journals (Sweden)

    S. Panneerselvam

    1987-10-01

    Full Text Available Aerodynamic configurations of tactical missiles have to produce the required lateral force with minimum time lag to meet the required manoeuvability and response time. The present design which is mainly based on linearised potential flow involves (a indentification of critical design points, (b design of lifting components and their integration with mutual interference, (c evaluation of aerodynamic characteristics, (d checking its adequacy at otherpoints, (e optimization of parameters and selection of configuration, and (f detailed evaluation including aerodynamic pressure distribution. Iterative design process in involed because of the mutual dependance between aerodynamic charactertistics and the parameters of the configuration. though this design method is based on third level of approximation with respect to real flow, aid of computer is essential for carrying out the iterative design process and also for effective selection of configuration by analysing performance. Futuristic design requirement which demand better accuracy on design and estimation calls for sophisticated super computer based theoretical methods viz. , full Euler solution/Navier-Strokes solutions.

  6. Bulkhead rupture disc for solid propellant missiles

    Energy Technology Data Exchange (ETDEWEB)

    Hibler, D.R. Sr.; Sigle, S.P. Jr.

    1988-04-19

    A missile bulkhead rupture disc assembly for disposition between a first stage of propellant and a second stage of propellant and for enabling release of the second stage of propellant subsequent to release of the first stage of propellant is described comprising: a generally circular element comprised of a frangible material and having a first burst pattern with a line of weakness completely circumscribing a central portion of the element. The central portion of the element having structure defines an aperture. The element has a second burst pattern comprising lines of weakness each extending in a substantially radial direction outwardly from the line of weakness of the first burst pattern. Each adjacent pair of the lines of weakness of the second burst pattern is spaced from each other and defines generally sector-shaped segments of the elements. The frangible material of the element has a tensile strength of a certain, first value in the vicinity of the line of weakness of the first burst pattern, and the frangible material of the element has a tensile strength in the vicinity of the lines of weakness of the second burst pattern of a second value which is higher than the first certain value.

  7. Ballistic versus diffusive transport in graphene

    Science.gov (United States)

    Borunda, Mario F.; Hennig, H.; Heller, Eric J.

    2013-09-01

    We investigate the transport of electrons in disordered and pristine graphene devices. Fano shot noise, a standard metric to assess the mechanism for electronic transport in mesoscopic devices, has been shown to produce almost the same magnitude (≈1/3) in ballistic and diffusive graphene devices and is therefore of limited applicability. We consider a two-terminal geometry where the graphene flake is contacted by narrow metallic leads. We propose that the dependence of the conductance on the position of one of the leads, a conductance profile, can give us insight into the charge flow, which can in turn be used to analyze the transport mechanism. Moreover, we simulate scanning probe microscopy (SPM) measurements for the same devices, which can visualize the flow of charge inside the device, thus complementing the transport calculations. From our simulations, we find that both the conductance profile and SPM measurements are excellent tools to assess the transport mechanism differentiating ballistic and diffusive graphene systems.

  8. Ballistic electron transport in wrinkled superlattices

    Science.gov (United States)

    Mitran, T. L.; Nemnes, G. A.; Ion, L.; Dragoman, Daniela

    2016-07-01

    Inspired by the problem of elastic wave scattering on wrinkled interfaces, we studied the scattering of ballistic electrons on a wrinkled potential energy region. The electron transmission coefficient depends on both wrinkle amplitude and periodicity, having different behaviors for positive and negative scattering potential energies. For scattering on potential barriers, minibands appear in the electron transmission, as in superlattices, whereas for scattering on periodic potential wells the transmission coefficient has a more complex form. Besides suggesting that tuning of electron transmission is possible by modifying the scattering potential via voltages on wrinkled gate electrodes, our results emphasize the analogies between ballistic electrons and elastic waves even in scattering problems on non-typical configurations.

  9. A ballistic motion disrupted by Bragg reflections

    CERN Document Server

    Clark, Jeremy Thane

    2012-01-01

    I study a Lindblad dynamics modeling a quantum test particle in a Dirac comb that collides with particles from a background gas. The main result is a homogenization theorem in a semi-classical limiting regime involving large mass for the test particle and a rescaling for the strength and period of the Dirac comb. Over the time interval considered, the particle would exhibit essentially ballistic motion if either the singular periodic potential or the kicks from the gas were removed. However, the particle behaves diffusively when both sources of forcing are present. The conversion of the motion from ballistic to diffusive is generated by occasional Bragg reflections that result when the test particle's momentum is driven through a collision near an element of the half-spaced reciprocal lattice of the Dirac comb.

  10. Ballistic model to estimate microsprinkler droplet distribution

    Directory of Open Access Journals (Sweden)

    Conceição Marco Antônio Fonseca

    2003-01-01

    Full Text Available Experimental determination of microsprinkler droplets is difficult and time-consuming. This determination, however, could be achieved using ballistic models. The present study aimed to compare simulated and measured values of microsprinkler droplet diameters. Experimental measurements were made using the flour method, and simulations using a ballistic model adopted by the SIRIAS computational software. Drop diameters quantified in the experiment varied between 0.30 mm and 1.30 mm, while the simulated between 0.28 mm and 1.06 mm. The greatest differences between simulated and measured values were registered at the highest radial distance from the emitter. The model presented a performance classified as excellent for simulating microsprinkler drop distribution.

  11. [Wound Ballistics – a Brief Overview].

    Science.gov (United States)

    Bolliger, Stephan A; Eggert, Sebastian; Thali, Michael J

    2016-02-01

    Wound ballistics examines the specific effect, namely the wound profile, of bullets on the body by firing at synthetic models made of ordnance gelatine, glycerin soap and synthetic bones, validated with real cases from (battlefield) surgery and forensic pathology. Wound profile refers to the penetration depth, the bullet deformation/ fragmentation, the diameter of the permanent and the temporary wound cavity. Knowing these features and the used ammunition a surgeon can rapidly assess the amount damage within a patient. The forensic pathologist can draw conclusions as to the used ammunition based on the wound profile. By measuring of the destructive capability of different ammunition types, wound ballistics lays the foundation for guidelines concerning the maximum effect of military ammunition. PMID:26837321

  12. A ballistic quantum ring Josephson interferometer

    International Nuclear Information System (INIS)

    We report the realization of a ballistic Josephson interferometer. The interferometer is made from a quantum ring etched in a nanofabricated two-dimensional electron gas confined in an InAs-based heterostructure laterally contacted to superconducting niobium leads. The Josephson current flowing through the structure shows oscillations with h/e flux periodicity when threading the loop with a perpendicular magnetic field. This periodicity, in sharp contrast with the h/2e one observed in conventional dc superconducting quantum interference devices, confirms the ballistic nature of the device in agreement with theoretical predictions. This system paves the way for the implementation of interferometric Josephson π-junctions, and for the investigation of Majorana fermions. (paper)

  13. Ballistic penetration of Perma-Gel

    Science.gov (United States)

    Ryckman, Raymond Albert; Powell, David Arthur; Lew, Adrian

    2012-03-01

    In this study a number of experiments were performed by taking high-speed footage of the firing spherical steel bullets at different speeds into Perma-Gel, a new synthetic thermoplastic material touted to exhibit similar properties to ordnance ballistic gelatin. We found that the gel undergoes very large and recoverable elastic deformations, which could strongly affect the dynamics of the temporary cavity formed behind the projectile. As with ordnance ballistic gelatin, the diameter of the temporary cavity can be many times the diameter of the projectile, in contrast with that of the permanent cavity which is several times smaller.We also observed that the closure of the cavity chokes the air inside, which could affect its dynamics in noticeable ways. Finally, one of the experiments suggest that the precise model of material failure may not be important to determine the dynamics of the temporary cavity.

  14. Ballistic Experiments with Titanium and Aluminum Targets

    Energy Technology Data Exchange (ETDEWEB)

    Gogolewski, R.; Morgan, B.R.

    1999-11-23

    During the course of the project we conducted two sets of fundamental experiments in penetration mechanics in the LLNL Terminal Ballistics Laboratory of the Physics Directorate. The first set of full-scale experiments was conducted with a 14.5mm air propelled launcher. The object of the experiments was to determine the ballistic limit speed of 6Al-4V-alloy titanium, low fineness ratio projectiles centrally impacting 2024-T3 alloy aluminum flat plates and the failure modes of the projectiles and the targets. The second set of one-third scale experiments was conducted with a 14.5mm powder launcher. The object of these experiments was to determine the ballistic limit speed of 6Al-4V alloy titanium high fineness ratio projectiles centrally impacting 6Al-4V alloy titanium flat plates and the failure modes of the projectiles and the target. We employed radiography to observe a projectile just before and after interaction with a target plate. Early on, we employed a non-damaging ''soft-catch'' technique to capture projectiles after they perforated targets. Once we realized that a projectile was not damaged during interaction with a target, we used a 4-inch thick 6061-T6-alloy aluminum witness block with a 6.0-inch x 6.0-inch cross-section to measure projectile residual penetration. We have recorded and tabulated below projectile impact speed, projectile residual (post-impact) speed, projectile failure mode, target failure mode, and pertinent comments for the experiments. The ballistic techniques employed for the experiments are similar to those employed in an earlier study.

  15. Highly efficient spin filtering of ballistic electrons

    Science.gov (United States)

    Steinmuller, S. J.; Trypiniotis, T.; Cho, W. S.; Hirohata, A.; Lew, W. S.; Vaz, C. A.; Bland, J. A.

    2004-04-01

    Spin dependent electron transport in hybrid Au/Co/Cu/NiFe/n-GaAs spin valve Schottky barrier structures was investigated using photoexcitation at various wavelengths. For excitation with the photon energy well above the Schottky barrier height we found a ˜2400% increase in helicity dependent photocurrent on switching the spin valve from parallel to antiparallel alignment. Our observations provide clear evidence for highly efficient spin filtering of spin polarized ballistic electrons.

  16. Modeling internal ballistics of gas combustion guns.

    Science.gov (United States)

    Schorge, Volker; Grossjohann, Rico; Schönekess, Holger C; Herbst, Jörg; Bockholdt, Britta; Ekkernkamp, Axel; Frank, Matthias

    2016-05-01

    Potato guns are popular homemade guns which work on the principle of gas combustion. They are usually constructed for recreational rather than criminal purposes. Yet some serious injuries and fatalities due to these guns are reported. As information on the internal ballistics of homemade gas combustion-powered guns is scarce, it is the aim of this work to provide an experimental model of the internal ballistics of these devices and to investigate their basic physical parameters. A gas combustion gun was constructed with a steel tube as the main component. Gas/air mixtures of acetylene, hydrogen, and ethylene were used as propellants for discharging a 46-mm caliber test projectile. Gas pressure in the combustion chamber was captured with a piezoelectric pressure sensor. Projectile velocity was measured with a ballistic speed measurement system. The maximum gas pressure, the maximum rate of pressure rise, the time parameters of the pressure curve, and the velocity and path of the projectile through the barrel as a function of time were determined according to the pressure-time curve. The maximum gas pressure was measured to be between 1.4 bar (ethylene) and 4.5 bar (acetylene). The highest maximum rate of pressure rise was determined for hydrogen at (dp/dt)max = 607 bar/s. The muzzle energy was calculated to be between 67 J (ethylene) and 204 J (acetylene). To conclude, this work provides basic information on the internal ballistics of homemade gas combustion guns. The risk of injury to the operator or bystanders is high, because accidental explosions of the gun due to the high-pressure rise during combustion of the gas/air mixture may occur. PMID:26239103

  17. Historical overview of wound ballistics research.

    Science.gov (United States)

    Maiden, Nick

    2009-01-01

    Ballistics involves the study of the scientific properties of projectiles, their behavior and their terminal effects on biological tissues and other materials. Wound ballistics deals with the analysis of injuries caused by projectiles and the behavior of projectiles within human or other biological tissues. The nineteenth century witnessed the development of both of these areas with Kocher's hydrodynamic theory and the understanding of the significance of bullet deformation in causing tissue injury. The degree of traumatic disruption of tissues and organs was also related to direct energy transfer from projectiles. While subsequent research has concentrated on elucidating further mechanisms of injury, the exact cause of remote tissue damage from high energy projectiles is still the subject of ongoing research. Much of the contemporary literature regarding wound ballistics concentrates on the forensic aspects and their application for legal purposes, in particular the investigation of shooting scenes. There have been many advances in this area, particularly in relation to the identification of various types of gunshot wounds and how their appearance can be used to establish if a shooting was accidental, deliberate (homicidal) or self inflicted (suicidal). PMID:19466590

  18. Targeting Low-Energy Ballistic Lunar Transfers

    Science.gov (United States)

    Parker, Jeffrey S.

    2010-01-01

    Numerous low-energy ballistic transfers exist between the Earth and Moon that require less fuel than conventional transfers, but require three or more months of transfer time. An entirely ballistic lunar transfer departs the Earth from a particular declination at some time in order to arrive at the Moon at a given time along a desirable approach. Maneuvers may be added to the trajectory in order to adjust the Earth departure to meet mission requirements. In this paper, we characterize the (Delta)V cost required to adjust a low-energy ballistic lunar transfer such that a spacecraft may depart the Earth at a desirable declination, e.g., 28.5(white bullet), on a designated date. This study identifies the optimal locations to place one or two maneuvers along a transfer to minimize the (Delta)V cost of the transfer. One practical application of this study is to characterize the launch period for a mission that aims to launch from a particular launch site, such as Cape Canaveral, Florida, and arrive at a particular orbit at the Moon on a given date using a three-month low-energy transfer.

  19. Wound ballistics of firearm-related injuries--part 1: missile characteristics and mechanisms of soft tissue wounding.

    Science.gov (United States)

    Stefanopoulos, P K; Filippakis, K; Soupiou, O T; Pazarakiotis, V C

    2014-12-01

    Firearm-related injuries are caused by a wide variety of weapons and projectiles. The kinetic energy of the penetrating projectile defines its ability to disrupt and displace tissue, whereas the actual tissue damage is determined by the mode of energy release during the projectile-tissue interaction and the particular characteristics of the tissues and organs involved. Certain projectile factors, namely shape, construction, and stability, greatly influence the rate of energy transfer to the tissues along the wound track. Two zones of tissue damage can be identified, the permanent cavity created by the passage of the bullet and a potential area of contused tissue surrounding it, produced mainly by temporary cavitation which is a manifestation of effective high-energy transfer to tissue. Due to the complex nature of these injuries, wound assessment and the type and extent of treatment required should be based on an understanding of the various mechanisms contributing to tissue damage. PMID:25128259

  20. Injuries of the head from backface deformation of ballistic protective helmets under ballistic impact.

    Science.gov (United States)

    Rafaels, Karin A; Cutcliffe, Hattie C; Salzar, Robert S; Davis, Martin; Boggess, Brian; Bush, Bryan; Harris, Robert; Rountree, Mark Steve; Sanderson, Ellory; Campman, Steven; Koch, Spencer; Dale Bass, Cameron R

    2015-01-01

    Modern ballistic helmets defeat penetrating bullets by energy transfer from the projectile to the helmet, producing helmet deformation. This deformation may cause severe injuries without completely perforating the helmet, termed "behind armor blunt trauma" (BABT). As helmets become lighter, the likelihood of larger helmet backface deformation under ballistic impact increases. To characterize the potential for BABT, seven postmortem human head/neck specimens wearing a ballistic protective helmet were exposed to nonperforating impact, using a 9 mm, full metal jacket, 124 grain bullet with velocities of 400-460 m/s. An increasing trend of injury severity was observed, ranging from simple linear fractures to combinations of linear and depressed fractures. Overall, the ability to identify skull fractures resulting from BABT can be used in forensic investigations. Our results demonstrate a high risk of skull fracture due to BABT and necessitate the prevention of BABT as a design factor in future generations of protective gear. PMID:25039407

  1. Impacts of Deflection Nose on Ballistic Trajectory Control Law

    OpenAIRE

    Bo Zhang; Shushan Wang; Mengyu Cao; Yuxin Xu

    2014-01-01

    The deflection of projectile nose is aimed at changing the motion of the projectile in flight with the theory of motion control and changing the exterior ballistics so as to change its range and increase its accuracy. The law of external ballistics with the deflectable nose is considered as the basis of the design of a flight control system and an important part in the process of projectile development. Based on the existing rigid external ballistic model, this paper establishes an external b...

  2. Some applications of ballistic electron emission microscopy/spectroscopy

    International Nuclear Information System (INIS)

    A brief review of ballistic electron emission microscopy and spectroscopy applications is presented. Results of our ballistic electron emission spectroscopy measurements on cleaved n-GaAs are given. The threshold in ballistic current-voltage characteristic is observed at bias 1.93 V which is high above the expected threshold. Explanation of this effect is given in the frame of present theoretical results. (author)

  3. Ballistic strength of woven fabrics for personal protection

    OpenAIRE

    Dimeski, Dimko; Spaseska, Dijana; Srebrenkoska, Vineta

    2009-01-01

    The purpose of the research was to make evaluation of the ballistic strength of four different fiber/resin composites intended to be used in manufacturing of ballistic items for personal protection. Research has been performed on glass, ballistic nylon, aramid and HPPE (High Performance Polyethylene) plain woven fabrics based composites. As a matrix system, in all cases, polyvinylbutyral modified phenolic resin was used. For the investigation, areal weight range 2-9 kg/m2, appl...

  4. Liquid Missile Fuels as Means of Chemical Terrorist Attack

    International Nuclear Information System (INIS)

    Modern world is faced with numerous terrorist attacks whose goals, methods and means of the conduct are various. It seems that we have entered the era when terrorism, one's own little terrorism, is the easiest and the most painless way of achieving a goal. That is why that such a situation has contributed to the necessity for strengthening individual and collective protection and safety, import and export control, control of the production and illegal sale of the potential means for delivering terrorist act. It has also contributed to the necessity for devising means of the delivery. For more than 10 years, a series of congresses on CB MTS Industry has pointed at chemicals and chemical industry as potential means and targets of terrorism. The specialization and experience of different authors in the field of the missile technology and missile fuels, especially those of Eastern origin, and the threat that was the reality of the war conflicts in 1990s was the reason for making a scientific and expert analysis of the liquid missile fuels as means of terrorism. There are not many experts in the field of NBC protection who are familiar with the toxicity and reaction of liquid missile fuels still lying discarded and unprotected in abandoned barracks all over Europe and Asia. The purpose of this paper is to draw public attention to possible different abuses of liquid missile fuels for a terrorist purpose, as well as to possible consequences and prevention measures against such abuses. (author)

  5. Missile launch detection electric field perturbation experiment. Final report

    Energy Technology Data Exchange (ETDEWEB)

    Kane, R.J.; Rynne, T.M.

    1993-04-28

    The Lawrence Livermore National Laboratory and SARA Inc. participated in the ATMD missile launch activities that occurred at WSMR during January 1993. LLNL and SARA deployed sensors for monitoring of basic phenomena. An attempt was made to measure perturbations of the earth geo-potential during the launch of a Lance missile. The occurrence of the perturbation is expected from the conducting body of the missile and the exhaust plume. A set of voltage-probe antennas were used to monitor the local electric field perturbation from the launch at ranges of approximately 1 km. Examination of the data acquired during the launch period failed to show identifiable correlation of the field variations with the launch event. Three reasons are ascribed to this lack of event data: (1) The electric field potential variations have a limited spatial correlation length - the fields measured in one region have little correlation to measurements made at distances of a kilometer away. The potential variations are related to localized atmospheric disturbances and are generally unpredictable. A value for the spatial correlation length is also not known. (2) The conductivity of the plume and missile body are not adequate to produce a field perturbation of adequate magnitude. Phenomena related to the exhaust plume and missile may exist and be outside of the collection range of the equipment employed for these measurements. (3) The presence of 60 Hz power line noise was of sufficient magnitude to irreversibly contaminate measurements.

  6. Cooled and uncooled infrared detectors for missile seekers

    Science.gov (United States)

    Fraenkel, Rami; Haski, Jacob; Mizrahi, Udi; Shkedy, Lior; Shtrichman, Itay; Pinsky, Ephi

    2014-06-01

    Electro-optical missile seekers pose exceptional requirements for infrared (IR) detectors. These requirements include: very short mission readiness (time-to-image), one-time and relatively short mission duration, extreme ambient conditions, high sensitivity, fast frame rate, and in some cases small size and cost. SCD is engaged in the development and production of IR detectors for missile seeker applications for many years. 0D, 1D and 2D InSb focal plane arrays (FPAs) are packaged in specially designed fast cool-down Dewars and integrated with Joule-Thomson (JT) coolers. These cooled MWIR detectors were integrated in numerous seekers of various missile types, for short and long range applications, and are combat proven. New technologies for the MWIR, such as epi-InSb and XBn-InAsSb, enable faster cool-down time and higher sensitivity for the next generation seekers. The uncooled micro-bolometer technology for IR detectors has advanced significantly over the last decade, and high resolution - high sensitivity FPAs are now available for different applications. Their much smaller size and cost with regard to the cooled detectors makes these uncooled LWIR detectors natural candidates for short and mid-range missile seekers. In this work we will present SCD's cooled and uncooled solutions for advanced electro-optical missile seekers.

  7. A synthesized windfield model for tornado missile transport

    International Nuclear Information System (INIS)

    A tornado windfield model has been developed for use in a probabilistic assessment of the tornado missile hazard to nuclear power plants. Tornado flow characteristics have been identified which are significant in terms of missile transport phenomena. In order to account for both modeling uncertainty and the natural variability observed among tornadoes, several random variables are specified in the model, including: tornado intensity, path width, translational speed, radius to maximum tangential velocity, ratio of radial-to-tangential wind speed, vertical variation of core size, and boundary layer thickness. Considering the lack of agreement regarding detailed tornado dynamics as well as the difficulty in establishing a priori conservative flow characteristics for missile transport, the windfield model was synthesized from theoretical, observational, and probabilistic considerations. A significant aspect of the model is that the parameters can be adjusted to make the intensity size and velocity variables consistent with the tornado path width boundary specification. The modelling considerations are discussed, the windfield model and calculational procedure presented, sample windfield component velocity profiles illustrated, and missile velocity statistics given for a simulation case study involving several thousand missile histories. (Auth.)

  8. Analysis of a Lance missile platoon using a semi-Markov chain

    OpenAIRE

    Argo, Harry M.

    1989-01-01

    Approved for public release; distribution is unlimited This thesis develops a combat effectiveness model for the Lance missile system. The survivability and ability to accomplish the mission for a Lance missile launch platoon depends upon enemy capabilities, platoon configuration, missile reliability and many other tangible factors. The changing status of a launch platoon is modeled using a semi-Markov chain with transient and absorbing states. Expected number of missiles fi...

  9. Design and Analysis of Missile Systems through CFD Simulations

    Science.gov (United States)

    Chakraborty, Debasis

    2010-10-01

    Development of indigenous CFD codes and their applications for complex aerodynamic and propulsive flow problems pertaining to DRDO missiles are presented. Grid generators, 3D Euler and Navier Stokes solvers are developed in-house using state of art numerical techniques and physical models. These softwares are used extensively for aerodynamic characterization of missiles over a wide range of Mach number, angle of attack, control surface deflection and store separation studies. Significant contributions are made in the design of high speed propulsion systems of various ongoing and future missiles through CFD analysis internal flow field. Important design modifications were suggested and the propulsion system performances were optimized. Capabilities have been developed for many advanced topics including computational aeroelasticity, coupled Euler Boltzmann solver, etc.

  10. Deflectable Nose Control for Bank-to-Turn Missile

    Institute of Scientific and Technical Information of China (English)

    WANG Xu-gang; ZHOU Jun; GUO Jian-guo; LIU Ji-zhong; GAO Xiao-ying

    2008-01-01

    It is an innovative try to control hypersonic bank-to-turn missiles using the deflectable nose and flaps. The high-er control efficiency, faster response, better stability and compactness of the nose control are shown by comparing the de-flectable nose control with the normal tail fin control. A mathematical model of the missile, which is time-varying, non-linear and strong coupling, is establihsed by multi-body dynamics to be used for designing the controller. A robust con-troller of deflectable nose control is designed by variable structure control theory, selecting sliding mode surfaces with tracking error and its integral function, and considering parameter disturbance of the model. The simulation results show the controller can response quickly and track precisely. The deflectable nose control is proper for the bank-to-turn missile.

  11. Online Guidance Law of Missile Using Multiple Design Point Method

    Science.gov (United States)

    Yamaoka, Seiji; Ueno, Seiya

    This paper deals with design procedure of online guidance law for future missiles that are required to have agile maneuverability. For the purpose, the authors propose to mount high power side-thrusters on a missile. The guidance law for such missiles is discussed from a point of view of optimal control theory in this paper. Minimum time problem is solved for the approximated system. It is derived that bang-bang control is optimal input from the necessary conditions of optimal solution. Feedback guidance without iterative calculation is useful for actual systems. Multiple design point method is applied to design feedback gains and feedforward inputs of the guidance law. The numerical results show the good performance of the proposed guidance law.

  12. Aerodynamic characteristics of missile configurations based on Soviet design concepts

    Science.gov (United States)

    Spearman, M. L.

    1979-01-01

    The aerodynamic characteristics of several missile concepts are examined. The configurations, which are based on some typical Soviet design concepts, include fixed-wing missiles with either forward- or aft-tail controls, and wing-control missiles with fixed aft stabilizing surfaces. The conceptual missions include air-to-air, surface-to-air, air-to-surface, and surface-to-surface. Analytical and experimental results indicate that through the proper shaping and location of components, and through the exploitation of local flow fields, the concepts provide generally good stability characteristics, high control effectiveness, and low control hinge moments. In addition, in the case of some cruise-type missions, there are indications of the application of area ruling as a means of improving the aerodynamic efficiency. In general, a point-design philosophy is indicated whereby a particular configuration is developed for performing a particular mission.

  13. High performance infrared fast cooled detectors for missile applications

    Science.gov (United States)

    Reibel, Yann; Espuno, Laurent; Taalat, Rachid; Sultan, Ahmad; Cassaigne, Pierre; Matallah, Noura

    2016-05-01

    SOFRADIR was selected in the late 90's for the production of 320×256 MW detectors for major European missile programs. This experience has established our company as a key player in the field of missile programs. SOFRADIR has since developed a vast portfolio of lightweight, compact and high performance JT-based solutions for missiles. ALTAN is a 384x288 Mid Wave infrared detector with 15μm pixel pitch, and is offered in a miniature ultra-fast Joule- Thomson cooled Dewar. Since Sofradir offers both Indium Antimonide (InSb) and Mercury Cadmium Telluride technologies (MCT), we are able to deliver the detectors best suited to customers' needs. In this paper we are discussing different figures of merit for very compact and innovative JT-cooled detectors and are highlighting the challenges for infrared detection technologies.

  14. Design Philosophy of variable Mass Preformed Fragmented Missile Warhead

    Directory of Open Access Journals (Sweden)

    K.P.S. Murthy

    1992-01-01

    Full Text Available Fragment hit density and hit probability of the warhead are the critical parameters in the selection of a preformed fragment-type missile warhead against ground targets. Hence these factors are to be maximised. The parametric studies of these factors have lead to a new concept of variable mass preformed fragmented (VMPF warhead. A philosophy was evolved for the VMPF-type missile warheads. A computer software for generating the external configuration of the VMPF-type missile warhead was developed and basic algorithm is discussed in this paper. With this new design approach, the fragment hit density and hit probability were improved considerably in the shorter ranges, when compared to that of a uniform mass preformed fragmented warhead of conventional design.

  15. Full-scale tornado-missile impact tests. Interim report

    International Nuclear Information System (INIS)

    Seven completed initial tests are described with 4 types of hypothetical tornado-borne missiles (impacting reinforced concrete panels that are typical of walls in nuclear power facilities). The missiles were rocket propelled to velocities currently postulated as being attainable by debris in tornadoes. (1500-pound 35-foot long utility pole; 8-pound 1-inch Grade 60 reinforcing bar; 78-pound 3-inch Schedule 40 pipe; and 743-pound 12-inch Schedule 40 pipe;) The results show that a minimum thickness of 24 inches is sufficient to prevent backface scabbing from normal impacts of currently postulated tornado missiles and that existing power plant walls are adequate for the most severe conditions currently postulated by regulatory agencies. This report gives selected detailed data on the tests completed thus far, including strain, panel velocity, and reaction histories

  16. The assessment of tornado missile hazard to nuclear power plants

    International Nuclear Information System (INIS)

    Numerical methods and computer codes for assessing tornado missile hazards to nuclear power plants are developed. The method of calculation has been based on the theoretical model developed earlier by authors. Historical data for tornado characteristics are taken from computerized files of the National Severe Storms Forecast Center and potential missiles characteristics are adopted from an EPRI report. Due to the uncertainty and randomness of tornado and tornado-generated missiles' characteristics, the damage probability of targets has highly spread distribution. The proposed method is very useful for assessing the risk of not providing protection to some nonsafety-related targets whose failure can create a hazard to the safe operation of nuclear power plants

  17. Full-scale tornado-missile impact tests. Final report

    International Nuclear Information System (INIS)

    The design of nuclear plant auxiliary building walls and roofs to resist impact from tornado-generated missiles has most recently been based on subscale data and empirical formulae derived from military tests of limited applicability. The test program described in the report provides data from full-scale simulated tornado-missile impacts of reinforced concrete walls that can be used directly for design. In addition, the data can be used to develop improved design and analysis techniques. This project is a part of an interdisciplinary program at EPRI aimed at providing a realistic basis for designing and analyzing nuclear power plants for the effects of hypothetical tornado-borne and in-plant missiles. The objective of the overall program is to ensure plant safety with efficient design

  18. Flexible missile autopilot design studies with PC-MATLAB/386

    Science.gov (United States)

    Ruth, Michael J.

    1989-01-01

    Development of a responsive, high-bandwidth missile autopilot for airframes which have structural modes of unusually low frequency presents a challenging design task. Such systems are viable candidates for modern, state-space control design methods. The PC-MATLAB interactive software package provides an environment well-suited to the development of candidate linear control laws for flexible missile autopilots. The strengths of MATLAB include: (1) exceptionally high speed (MATLAB's version for 80386-based PC's offers benchmarks approaching minicomputer and mainframe performance); (2) ability to handle large design models of several hundred degrees of freedom, if necessary; and (3) broad extensibility through user-defined functions. To characterize MATLAB capabilities, a simplified design example is presented. This involves interactive definition of an observer-based state-space compensator for a flexible missile autopilot design task. MATLAB capabilities and limitations, in the context of this design task, are then summarized.

  19. 76 FR 63541 - Design-Basis Hurricane and Hurricane Missiles for Nuclear Power Plants

    Science.gov (United States)

    2011-10-13

    ... COMMISSION 10 CFR Parts 50 and 52 Design-Basis Hurricane and Hurricane Missiles for Nuclear Power Plants... Hurricane and Hurricane Missiles for Nuclear Power Plants.'' This regulatory guide provides licensees and...- basis hurricane and design-basis hurricane-generated missiles that a nuclear power plant should...

  20. Heat Transfer Between a Missile's Combustion Chamber and the Warhead

    Institute of Scientific and Technical Information of China (English)

    赵永涛; 张奇; 白春华; 闫华

    2003-01-01

    Under higher temperatures the charge within a warhead will be subjected to physical and chemical changes, which will influence the security of the warhead launching process. In this paper the problem is studied adopting finite difference method for the case of a rocket-powered missile. Temperature distribution tables are given through quadrature experiments, and the results fit the actual measured values very well. The results also show that to ensure the launching security of rocket-powered missiles having warhead charge critical temperature close to about 60 ℃, the designer can select appropriate heat insulation structural parameters.

  1. Robust controller design for a skid to turn missile

    Science.gov (United States)

    Sreenatha, A. G.; Rajhans, Vivek; Bhardwaj, Neeraj

    1999-11-01

    The design and analysis of Robust Autopilot for skid-to-turn missile is presented. Two of the popular Robust Controller design approaches, The Loop Shaping Design Procedure (LSDP) and The Robust Eigenstructure Assignment are considered. The missile model considered in the present work is having lightly damped modes and non-minimum phase zeros, with stringent performance requirements. Numerical results are presented to evaluate the Robustness of stability and performance of the controller. Merits and demerits of the above said methodologies are brought out clearly as applied to this specific plant.

  2. Electric Loading Simulation System for Missile Wings and Rudders

    Institute of Scientific and Technical Information of China (English)

    QI Rong; LIN Hui; CHEN Ming

    2006-01-01

    The design and the realization of missile wings and rudders loading simulation system based on digital signal processor (DSP) TMS320LF2407 and direct torque control (DTC) servo driver ACS600 are discussed. The structure and opration principle for the system are presented. Speediness and elimination of superabundant torque are two key difficulties for electric loading simulation system. The method which can eliminate the superabundant torque is researched. Test results show the airflow resistance when missile wings and rudders are spreading can be rapidly simulated with high accuracy.

  3. A METHOD IN SYSTEM DESIGN OF EJECTING DEVICES OF MISSILES

    Institute of Scientific and Technical Information of China (English)

    DaiLongcheng; XuanYimin

    2002-01-01

    Anew method in system design of ejecting devices of missiles is first presented.Some important points are dis-cussed,which guid the research and development of new ejecting devices of missileg,amd provid the foundation flr thw design of mew ejecting device is provided.The system design includes the distribution of techmology specifica-tion,3-D solid modeling of ejecting devices of missiles im-ported from abroad,the design of pmeumatic device sys-tem,the design of ejecting mechanism system,the predic-tion of reliability and the experimental analysis,etc.

  4. Internal Ballistic Code for Solid Rocket Motors using Minimum Distance Function for Grain Burnback

    Directory of Open Access Journals (Sweden)

    Afroz Javed

    2015-05-01

    Full Text Available A computer code has been developed for internal ballistic performance evaluation of solid rocket motors, using minimum distance function (MDF approach for prediction of geometry evolution. This method can handle any complex geometry without the need to define different geometrical shapes and their evolution as used in several existing analytical geometry evolution-based methodologies. The code is validated with both experimental results published in literature, as well as for solid rocket motors of tactical and strategic missiles and a very good match is obtained with static test results. The output of the code gives p-t (pressure-time curve as well as the detailed parameters of the flow along the axial direction, and geometries in the form of mesh file, which can be further used as input to codes for CFD analysis.Defence Science Journal, Vol. 65, No. 3, May 2015, pp.181-188, DOI: http://dx.doi.org/10.14429/dsj.65.8304

  5. Ballistic thermoelectric properties in boron nitride nanoribbons

    Science.gov (United States)

    Xie, Zhong-Xiang; Tang, Li-Ming; Pan, Chang-Ning; Chen, Qiao; Chen, Ke-Qiu

    2013-10-01

    Ballistic thermoelectric properties (TPs) in boron nitride nanoribbons (BNNRs) are studied using the nonequilibrium Green's function atomistic simulation of electron and phonon transport. A comparative analysis for TPs between BNNRs and graphene nanoribbons (GNRs) is made. Results show that the TPs of BNNRs are better than those of GNRs stemming from the higher power factor and smaller thermal conductance of BNNRs. With increasing the ribbon width, the maximum value of ZT (ZTmax) of BNNRs exhibits a transformation from the monotonic decrease to nonlinear increase. We also show that the lattice defect can enhance the ZTmax of these nanoribbons strongly depending on its positions and the edge shape.

  6. Narrow electron injector for ballistic electron spectroscopy

    International Nuclear Information System (INIS)

    A three-terminal hot electron transistor is used to measure the normal energy distribution of ballistic electrons generated by an electron injector utilizing an improved injector design. A triple barrier resonant tunneling diode with a rectangular transmission function acts as a narrow (1 meV) energy filter. An asymmetric energy distribution with its maximum on the high-energy side with a full width at half maximum of ΔEinj=10 meV is derived. [copyright] 2001 American Institute of Physics

  7. Going ballistic: Graphene hot electron transistors

    Science.gov (United States)

    Vaziri, S.; Smith, A. D.; Östling, M.; Lupina, G.; Dabrowski, J.; Lippert, G.; Mehr, W.; Driussi, F.; Venica, S.; Di Lecce, V.; Gnudi, A.; König, M.; Ruhl, G.; Belete, M.; Lemme, M. C.

    2015-12-01

    This paper reviews the experimental and theoretical state of the art in ballistic hot electron transistors that utilize two-dimensional base contacts made from graphene, i.e. graphene base transistors (GBTs). Early performance predictions that indicated potential for THz operation still hold true today, even with improved models that take non-idealities into account. Experimental results clearly demonstrate the basic functionality, with on/off current switching over several orders of magnitude, but further developments are required to exploit the full potential of the GBT device family. In particular, interfaces between graphene and semiconductors or dielectrics are far from perfect and thus limit experimental device integrity, reliability and performance.

  8. MD Test of a Ballistic Optics

    CERN Document Server

    Garcia-Tabares Valdivieso, Ana; Salvachua Ferrando, Belen Maria; Skowronski, Piotr Krzysztof; Solfaroli Camillocci, Matteo; Tomas Garcia, Rogelio; Wenninger, Jorg; Coello De Portugal - Martinez Vazquez, Jaime Maria; CERN. Geneva. ATS Department

    2016-01-01

    The ballistic optics is designed to improve the understanding of optical errors and BPM systematic effects in the critical triplet region. The particularity of that optics is that the triplet is switched off, effectively transforming the triplets on both sides of IR1 and IR5 into drift spaces. Advantage can be taken from that fact to localize better errors in the Q4-Q5-triplet region. During this MD this new optics was tested for the first time at injection with beam 2.

  9. Real-world ballistics: A dropped bucket

    OpenAIRE

    Hogg, David W.

    2007-01-01

    I discuss an apparently simple ballistics problem: the time it takes an object to fall a small vertical distance near the surface of the Earth. It turns out to be not so simple; I spend a great deal of time on the quantitative assessment of the assumptions involved, especially with regards to the influence of the air. The point is \\emph{not} to solve the problem; indeed I don't even end up solving the problem exactly. I introduce dimensional analysis to perform all of the calculations approxi...

  10. Towards reliable simulations of ballistic impact on concrete structures

    NARCIS (Netherlands)

    Khoe, Y.S.; Tyler Street, M.D.; Maravalalu Suresh,, R.S.; Weerheijm, J.

    2013-01-01

    Protection against weapon effects like ballistic impacts, fragmenting shells and explosions is the core business of the Explosions, Ballistics and Protection department of TNO (The Netherlands). Experimental and numerical research is performed to gain and maintain the knowledge to support the Dutch

  11. Sub-ballistic behavior in the quantum kicked rotor

    International Nuclear Information System (INIS)

    We study the resonances of the quantum kicked rotor subjected to an excitation that follows an aperiodic Fibonacci prescription. In such a case the secondary resonances show a sub-ballistic behavior like the quantum walk with the same aperiodic prescription for the coin. The principal resonances maintain the well-known ballistic behavior

  12. Comments on "Ballistics: a primer for the surgeon"

    OpenAIRE

    Courtney, Michael; Courtney, Amy

    2008-01-01

    In response to a published assertion to the contrary, this paper briefly reviews many studies that document remote wounding effects of ballistic pressure waves including experiments in pigs and dogs that find brain injury resulting from animal models shot in the thigh and case studies in humans that document both remote brain and spinal cord injuries ascribed to ballistic pressure waves.

  13. Development and testing of a flexible ballistic neck protection

    NARCIS (Netherlands)

    Roebroeks, G.H.J.J.; Rensink, P.

    2016-01-01

    Sufficient ballistic protection of the neck area would significantly reduce the vulnerability of an infantry soldier. So far this protection is offered by extensions on the ballistic vest or combat helmet. However, the requirements for head agility and the various body to head positions combined wit

  14. Ballistic performance and microstructure of four armor ceramics

    NARCIS (Netherlands)

    Abadjieva, E.; Carton, E.P.

    2013-01-01

    The ballistic behavior of four different armor ceramic materials with thicknesses varying from 3 mm to 14 mm has been investigated. These are two types of alumina Al2O3 armor grades and two types of SiC armor grades produced by different armor ceramic producers. The ballistic study has been performe

  15. Heat spike and ballistic contributions to mixing in Si

    International Nuclear Information System (INIS)

    We have studied atomic mixing in silicon by the classical molecular dynamics method, and directly compared the simulated data to experimental measurements. The relative importance of ballistic collisions and heat spike to the mixing is considered. We obtain a fairly good agreement between experiments and simulations. The heat spike contribution to the total mixing seems to be much lower than that of ballistic collisions

  16. Patriot missile defense systems might be deployed in Baltics - German general

    Index Scriptorium Estoniae

    2016-01-01

    Saksamaa ja Holland testivad oktoobris Patriot-tüüpi rakette. Saksa brigaadikindral Michael Gschossmanni sõnul võidakse testimisele tulevaid õhutõrjesüsteeme paigutada tulevikus Balti riikidesse või Poola

  17. Tornado missile simulation and design methodology. Volume 2: model verification and data base updates. Final report

    Energy Technology Data Exchange (ETDEWEB)

    Twisdale, L.A.; Dunn, W.L.

    1981-08-01

    A probabilistic methodology has been developed to predict the probabilities of tornado-propelled missiles impacting and damaging nuclear power plant structures. Mathematical models of each event in the tornado missile hazard have been developed and sequenced to form an integrated, time-history simulation methodology. The models are data based where feasible. The data include documented records of tornado occurrence, field observations of missile transport, results of wind tunnel experiments, and missile impact tests. Probabilistic Monte Carlo techniques are used to estimate the risk probabilities. The methodology has been encoded in the TORMIS computer code to facilitate numerical analysis and plant-specific tornado missile probability assessments.

  18. Strategy missile control system design using adaptive fuzzy control based on Popov stability criterion

    Science.gov (United States)

    Zhang, Jianling; An, Jinwen; Wang, Mina

    2005-11-01

    This paper describes the application and simulation of an adaptive fuzzy controller for a missile model. The fuzzy control system is tested using different values of fuzzy controller correctional factor on a nonlinear missile model. It is shown that the self-tuning fuzzy controller is well suited for controlling the pitch loop of the missile control system with air turbulence and parameter variety. The research shows that the Popov stability criterion could successfully guarantee the stability of the fuzzy system. It provides a good method for the design of missile control system. Simulation results suggest significant benefits from fuzzy logic in control task for missile pitch loop control.

  19. Design and Implementation of One Missile Visual Simulation System Based on OpenGL

    Institute of Scientific and Technical Information of China (English)

    GAO Ying; ZHANG Pu-zhao; PENG Yu-xin; HUANG Jian-guo

    2007-01-01

    The implementation of a missile's visual simulation system is explained that is developed with OpenGL(open graphic library) and the flight path and flight carriage in different stages of the missile are displayed. The establishment problems of the 3D scene are circumstantiated including the construction and redeployment of the model, creation of the virtual scene, setting of the multi-viewports and multi-windows etc. The missile's data driver, system flow, the modules and their mutual relations of the missile visual simulation system are discussed. The missile flight simulation results and effect of the scenes are given.

  20. Local damage to Ultra High Performance Concrete structures caused by an impact of aircraft engine missiles

    Energy Technology Data Exchange (ETDEWEB)

    Riedel, Werner [Fraunhofer Institute for High-Speed Dynamics, Ernst-Mach-Institute, Eckerstrasse 4, D-79104 Freiburg (Germany); Noeldgen, Markus, E-mail: mnoeldgen@schuessler-plan.d [Fraunhofer Institute for High-Speed Dynamics, Ernst-Mach-Institute, Eckerstrasse 4, D-79104 Freiburg (Germany); Schuessler-Plan Engineering Ltd., St.-Franziskus-Str. 148, D-40470 Duesseldorf (Germany); Strassburger, Elmar; Thoma, Klaus [Fraunhofer Institute for High-Speed Dynamics, Ernst-Mach-Institute, Eckerstrasse 4, D-79104 Freiburg (Germany); Fehling, Ekkehard [University of Kassel, Chair of Structural Concrete, Kurt-Wolters Str. 3, D-34109 Kassel (Germany)

    2010-10-15

    Research highlights: {yields} Experimental series on UHPC panels subjected to aircraft engine impact. {yields} Improved ballistic limit of fiber reinforced UHPC in comparison to conventional R/C. {yields} Detailed investigation of failure mechanisms of fiber reinforced UHPC panel. - Abstract: The impact of an aircraft engine missile causes high stresses, deformations and a severe local damage to conventional reinforced concrete. As a consequence the design of R/C protective structural elements results in components with rather large dimensions. Fiber reinforced Ultra High Performance Concrete (UHPC) is a concrete based material which combines ultra high strength, high packing density and an improved ductility with a significantly increased energy dissipation capacity due to the addition of fiber reinforcement. With those attributes the material is potentially suitable for improved protective structural elements with a reduced need for material resources. The presented paper reports on an experimental series of scaled aircraft engine impact tests with reinforced UHPC panels. The investigations are focused on the material behavior and the damage intensity in comparison to conventional concrete. The fundamental work of is taken as reference for the evaluation of the results. The impactor model of a Phantom F4 GE-J79 engine developed and validated by Sugano et al. is used as defined in the original work. In order to achieve best comparability, the experimental configuration and method are adapted for the UHPC experiments. With 'penetration', 'scabbing' and 'perforation' all relevant damage modes defined in are investigated so that a full set of results are provided for a representative UHPC structural configuration.

  1. Task Programming of Antiballistic Missile Sensors Based on MAS%基于多智能体的反导传感器任务规划算法

    Institute of Scientific and Technical Information of China (English)

    吴林锋; 王刚; 刘昌云; 杨少春

    2012-01-01

    The characteristics and functions of the sensor resources under the antiballistic missile condition are firstly discussed, Then a sensor task programming system structure which adapts to the anti-ballistic missile requirement is put forward based on the multi-agent system (MAS) of distribute artificial intelligence, and the main functions of each agent in the structure in detail is analyzed. Finally a programming process is presented and the arithmetic of a sensor Agent in the layer of entity is carried out, which provides an effective method for building a high-efficiency and intelligent antimissile sensor network.%首先探讨了反导作战中各类传感器资源的构成特点和功能划分,然后基于多智能体multy-agent system(MAS)的分布式人工智能技术提出了适应反导作战需求的传感器任务规划体系架构,既而深入分析了体系架构中各类agent的主要功能,最后给出了一个实体层传感器的任务规划流程和算法实例,为构建高效率、智能化的反导作战多传感器任务规划技术提供了一种有效的研究方法.

  2. Simulation Modeling Technique of Kinetic Missile Impact Probability on Target%动能拦截弹弹目碰撞概率仿真建模技术

    Institute of Scientific and Technical Information of China (English)

    郭宁; 姬聪生

    2011-01-01

    针对目前研究反导拦截的主要方式——直接碰撞杀伤技术,提出了一种动能拦截弹弹目碰撞计算模型用以进行动能拦截弹与目标碰撞的概率计算,拦截弹碰撞目标的要害部位分析以及不同交会姿态对碰撞概率的影响分析.此模型是直接动能杀伤目标毁伤评估建模的基础,也可用于对拦截弹最佳碰撞方式的研究等方面.%According to the main method of research of intercepting tactical ballistic missile ( TBM ) hit-to-kill technology, a model for the computation of the missile-target collision probability of kinetic kill vehicle (KKV) and TBM is proposed. TBM vital part collided with KKV and the collision probability caused by different attitude are analyzed. The model is the damage assessment modeling base of hit-to-kill technology and can also be used for the research of the best way of the KKV s collision.

  3. An analysis of the common missile and TOW 2B on the Stryker anti-tank guided missile platform, using the Janus simulation

    OpenAIRE

    Peterson, Samuel L.

    2002-01-01

    The U.S. Army is beginning to field the first of six Stryker Brigade Combat Teams (SBCTs) and equip the organic Anti-Tank (AT) Company of the Brigade with the LAV III Anti-Tank Guided Missile (ATGM) Platform and the Tube-Launched, Optically-Tracked, Wire-Guided 2B (TOW 2B) missile system. A developmental effort is currently underway to replace the aging TOW 2B and Hellfire missile systems with a common missile that meets both ground and air requirements. With increased range, lethality, and...

  4. Micro-electro-mechanical system (MEMS) component research and development for army missile applications

    Science.gov (United States)

    Hudson, Tracy D.; McMillen, Deanna K.; Ashley, Paul R.; Ruffin, Paul B.; Baeder, Janet

    1999-07-01

    The US Army Aviation and Missile Command Missile Research, Development and Engineering Center has identified MEMS as an emerging technology with high potential for fulfilling the mission of future missiles. The technology holds the promise of reducing the size, weight, cost, and power requirements for performing existing functions in Army missile systems, as well las providing opportunities for new computing, sensing, and actuation functions that cannot be achieved with conventional electromechanical technology. MEMS will enable the Army's next generation of smaller and lighter missiles. The military market drives the thrust for development of miniature sensor with applications such as: competent and smart munitions, aircraft and missile autopilots, tactical missile guidance, fire control system, platform stabilization, smart structures with embedded inertial sensors, missile system health monitoring, missile and ground-based radar, radio frequency seekers, aerodynamic flow control, IR imagers, and multiple intelligent small projectiles. Current efforts at AMCOM include the development of MEMS-based inertial components to include accelerometers with wide dynamic range, tactical grade gyros with high rate range, and miniature three-axis inertial measurement unit with common interface electronics. Performance requirements of such components will be presented in terms of current and future Army missile systems. Additional MEMS based efforts under investigation at AMCOM include missile storage health monitoring, RF MEMS components, encoders for actuators, and aerodynamic flow control will also be discussed.

  5. 22 CFR 121.16 - Missile Technology Control Regime Annex.

    Science.gov (United States)

    2010-04-01

    ... missile systems, see § 121.1, Cat. VIII (a), target drones and reconnaissance drones (see § 121.1, Cat... assemblies and components specifically designed for military use and operation at temperatures in excess of...: (a) Designed to meet military specifications for ruggedized equipment (see § 121.1, Category...

  6. External interaction of the nuclear EMP with aircraft and missiles

    International Nuclear Information System (INIS)

    The general problem of external coupling of the nuclear EMP to metal structures is discussed with attention directed toward aircraft and missiles. Theoretical and experimental data are presented fo the skin current and charge densities induced on aircraft. Recommendations for future studies are also given

  7. Shipborne Laser Beam Weapon System for Defence against Cruise Missiles

    Directory of Open Access Journals (Sweden)

    J.P. Dudeja

    2000-04-01

    Full Text Available Sea-skim~ing cruise missiles pose the greatest threat to a surface ship in the present-day war scenario. The convenitional close-in-weapon-systems (CIWSs are becoming less reliable against these new challenges requiring extremely fast reaction time. Naval Forces see a high energy laser as a feasible andjeffective directed energy weapon against sea-skimming antiship cruise missiles becauseof its .ability to deliver destructive energy at the speed of light on to a distant target. The paper comparesthe technology and capability of deuterium fluoride (DF and chemical-oxygen-iodine laser (COIL in effectively performing the role of a shipborne CIWS altainst sea-skimming missiles. Out of these twolasers, it is argued that DF laser wo.uld be more effective a,s a shipborne weapon for defence against sea-skimmin,g cruise missiles. Besides the high energy laser as the primary (killing laser, othersub-systems required in the complete weapon system would be: A beacon laser to sense phase distor'ions in the primary laser, adaptive optics to compensate the atmospheric distortions, beam-directing optics, illuminating lasers, IRST sensors, surveillance and tracking radars, interfacing system, etc.

  8. Theoretical study of self-balancing missiles. [design for maximum vertical or lateral accelerations

    Science.gov (United States)

    Hopkins, E. J.

    1976-01-01

    A theoretical study based on linear theory is presented for two types of 'self-balancing' missiles, designed to accelerate vertically or laterally without pitching or yawing. One type of missile had a variable-incidence wing and the other type had wing flaps to provide acceleration. The main objective of this investigation is to compare the maximum available acceleration for these self-balancing missiles with that of conventional pitching-type missiles. Ten different configurations were considered. The results indicate that self-balancing missiles with either variable wing incidence or wing flaps are feasible, but that the maximum available acceleration for these missiles is less than for a conventional pitching-type missile having the same wing and tail surfaces.

  9. Hardware in Loop Simulation for Missile Guidance and Control Systems

    Directory of Open Access Journals (Sweden)

    S. K. Chaudhuri

    1997-07-01

    Full Text Available The purpose of the guidance law is to determine appropriate missile flight path dynamics to achieve mission objective in an efficient manner based on navigation information. Today, guided missiles which are aerodynamically unstable or non-linear in all or part of the flight envelopes need control systems for stability as well as for steering. Many classical guidance and control laws have been used for tactical missiles with varying degrees of performance, complexity and seeker/sensor requirements. Increased accuracy requirements and more dynamic tactics of modern warfare demand improvement of performance which is a trade-off between sophisticated hardware and more sophisticated software. To avoid increase in cost by hardware sophistication, today's trend is to exploit new theoretical methods and low cost high speed microprocessor techniques. Missile test flights are very expensive. The missile system with its sophisticated software and hardware is not reusable after a test launch. Hardware-in-loop Simulation (HILS facilities and methodology form a well integrated system aimed at transforming a preliminary guidance and control system design to flight software and hardware with trajectory right from lift-off till its impact. Various guidance and control law studies pertaining to gathering basket and stability margins, pre-flight, post-flight analyses and validation of support systems have been carried out using this methodology. Nearly full spectrum of dynamically accurate six-degrees-of-freedom (6-DOF model of missile systems has been realised in the HILS scenario. The HILS facility allows interconnection of missile hardware in flight configuration. Pre-flight HILS results have matched fairly well with actual flight trial results. It was possible to detect many hidden defects in the onboard guidance and control software as well as in hardware during HILS. Deficiencies in model, like tail-wag-dog (TWD, flexibility, seeker dynamics and defects in

  10. Pricing Strategy, Pricing Stability and Financial Condition in the Defense Aerospace Industry

    OpenAIRE

    Johnstone, Jeffrey Carl; Keavney, Patrick Daniel

    1987-01-01

    Approved for public release, distribution unlimited The purpose of this research is to determine if pricing strategy and pricing stability for products in the defense aerospace industry can be predicted based on a firm's financial condition. The sample for this research includes 17 contractors and 52 missile and aircraft programs. Two separate issues are addressed. The first issue concerns the relationship between financial condition and contractor pricing strategy. The second concerns the...

  11. Ballistic Limit Equation for Single Wall Titanium

    Science.gov (United States)

    Ratliff, J. M.; Christiansen, Eric L.; Bryant, C.

    2009-01-01

    Hypervelocity impact tests and hydrocode simulations were used to determine the ballistic limit equation (BLE) for perforation of a titanium wall, as a function of wall thickness. Two titanium alloys were considered, and separate BLEs were derived for each. Tested wall thicknesses ranged from 0.5mm to 2.0mm. The single-wall damage equation of Cour-Palais [ref. 1] was used to analyze the Ti wall's shielding effectiveness. It was concluded that the Cour-Palais single-wall equation produced a non-conservative prediction of the ballistic limit for the Ti shield. The inaccurate prediction was not a particularly surprising result; the Cour-Palais single-wall BLE contains shield material properties as parameters, but it was formulated only from tests of different aluminum alloys. Single-wall Ti shield tests were run (thicknesses of 2.0 mm, 1.5 mm, 1.0 mm, and 0.5 mm) on Ti 15-3-3-3 material custom cut from rod stock. Hypervelocity impact (HVI) tests were used to establish the failure threshold empirically, using the additional constraint that the damage scales with impact energy, as was indicated by hydrocode simulations. The criterion for shield failure was defined as no detached spall from the shield back surface during HVI. Based on the test results, which confirmed an approximately energy-dependent shield effectiveness, the Cour-Palais equation was modified.

  12. Materials Database Development for Ballistic Impact Modeling

    Science.gov (United States)

    Pereira, J. Michael

    2007-01-01

    A set of experimental data is being generated under the Fundamental Aeronautics Program Supersonics project to help create and validate accurate computational impact models of jet engine impact events. The data generated will include material property data generated at a range of different strain rates, from 1x10(exp -4)/sec to 5x10(exp 4)/sec, over a range of temperatures. In addition, carefully instrumented ballistic impact tests will be conducted on flat plates and curved structures to provide material and structural response information to help validate the computational models. The material property data and the ballistic impact data will be generated using materials from the same lot, as far as possible. It was found in preliminary testing that the surface finish of test specimens has an effect on measured high strain rate tension response of AL2024. Both the maximum stress and maximum elongation are greater on specimens with a smoother finish. This report gives an overview of the testing that is being conducted and presents results of preliminary testing of the surface finish study.

  13. Ballistic electron spectroscopy of semiconductor heterostructures

    International Nuclear Information System (INIS)

    A systematic study of electron transport through semiconductor superlattices in the transition region between coherent and scattering induced transport is performed. The measurements are carried out using a hot electron transistor as an electron spectrometer. A quasi monoenergetic, variable energy, ballistic hot electron beam is generated by a tunneling barrier injector and used to probe the intrinsic heterostructure transport properties as a function of a uniform electric field. Under flat band conditions the eigenstates of a periodic structure extend over the entire length of the superlattice forming minibands. From the measured transfer ratios, miniband positions and miniband widths are determined and compared to the results from self consistent calculations. The transmittance of the superlattice at different superlattice bias conditions is measured by varying the energy of the injected hot electron beam. For a superlattice longer than the coherence length, the transmission becomes asymmetric and dependent on the electric field direction. The onset of scattering induced miniband transport is clearly evident and the transition between coherent and incoherent electron transport in superlattices is observed for the first time. A coherence length of 150 nm and a scattering time of 1 ps is determined. The experimental result is in good agreement to a fully three dimensional calculation including interface roughness with typical island sizes of 10 mn. This clearly demonstrates that interface roughness scattering limits the coherence length of ballistic electrons in the superlattice. (author)

  14. Short report of an unusual ballistic trauma

    Science.gov (United States)

    Inchingolo, Francesco; Tatullo, Marco; Marrelli, Massimo; Inchingolo, Alessio D.; Pinto, Giorgia; Inchingolo, Angelo M.; Dipalma, Gianna

    2011-01-01

    INTRODUCTION Portable firearms have a relevant medico-legal interest, being a major cause of injury. Bullet entry wounds generally have a particular appearance, including contusion, skin introflection, and simple or excoriated ecchymosis. The skin wound is typically a hole with frayed margins, whose diameter is smaller than that of the bullet. PRESENTATION OF CASE We report the case of a 19-year-old man with ballistic trauma. Examination of the patient's lesions indicated that the bullet had entered from the left mandibular parasymphysis, creating a small hole without the typical bullet wipe and blackening. Subsequently, the bullet seemed to have fractured the left chin region immediately below the lower alveolar process, and it finally stopped in the submandibular area in the suprahyoid region of the neck. DISCUSSION This case is peculiar because the distinctive features of a firearm injury were absent; the lack of bleeding and edema made the case difficult to interpret without additional diagnostic investigations. CONCLUSION Ballistic trauma can manifest in different ways; therefore, internal trauma should be suspected even in the absence of clear external signs. This case report shows how an unusual bullet entry hole can mask quite serious injuries. PMID:22096751

  15. Understanding Defense Mechanisms.

    Science.gov (United States)

    Cramer, Phebe

    2015-12-01

    Understanding defense mechanisms is an important part of psychotherapy. In this article, we trace the history of the concept of defense, from its origin with Freud to current views. The issue of defense as an unconscious mechanism is examined. The question of whether defenses are pathological, as well as their relation to pathology, is discussed. The effect of psychotherapy on the use of defenses, and their relation to a therapeutic alliance is explored. A series of empirical research studies that demonstrate the functioning of defense mechanisms and that support the theory is presented. Research also shows that as part of normal development, different defenses emerge at different developmental periods, and that gender differences in defense use occur. PMID:26583439

  16. Study on Titanium Alloy TC4 Ballistic Penetration Resistance Part Ⅰ: Ballistic Impact Tests

    Institute of Scientific and Technical Information of China (English)

    ZHANG Tao; CHEN Wei; GUAN Yupu; GAO Deping

    2012-01-01

    Ballistic impact test of different-scale casings is an efficient way to demonstrate the casing containment capability at the preliminary design stage of the engine.For the sake of studying the titanium alloy TC4 casing performance,the ballistic tests of flat and curved simulation casing are implemented by using two flat blades of different sizes as the projectile.The impact mechanism and failure of the target are discussed.Impact of the projectile is a highly nonlinear transient process with the large deformation of the target.On the impact,failures of the flat casing and the subscale casing are similar,concluding two parts,the global dishing and localized ductile tearing.The main localized failure mode combines plugging (shear) and petaling (shear) if the projectile perforates or penetrates,while crater (shear) if the projectile rebounds.The ballistic limit equation is verified by the test data and the results show that this empirical equation could be a practical way to estimate the critical velocity.

  17. Laminated metals composites fracture and ballistic impact behavior

    Energy Technology Data Exchange (ETDEWEB)

    Lesuer, D.R.; Syn, C.K.; Sherby, O.D.; Wadsworth, J.

    1998-01-20

    Recent advances in the fracture and ballistic impact response of laminated metal composites (LMCs) are reviewed. The laminate structure can provide significant improvements to these properties relative to the component materials. Typical fracture and ballistic impact properties in LMCs are illustrated for systems containing Al alloys and Al matrix composites. The unique mechanisms operating in a layered structure that contribute to fracture or ballistic impact resistance are discussed. The influence of laminate architecture, component material properties and interface strength on mechanisms and properties are briefly reviewed for these Al-based LMCs.

  18. Effect of Clamping Rigidity of the Armour on Ballistic Performance

    Directory of Open Access Journals (Sweden)

    S. N. Dikshit

    1992-04-01

    Full Text Available Influence of the manner in which the armour plates are held during their ballistic testing on the armour performance, has been evaluated. One armour plate was clamped rigidly to the test stand while a second plate of identical composition, hardness, and dimensions was hung loosely from the target holder. Both these plates were impacted with the same type of projectiles and over the same impact velocity range. The nature of ballistic damage evaluated indicates that the manner in which the armour is held during ballistic testing has a negligible influence on its performance at least when the mass of the plate is substantially higher than that of the projectile.

  19. Ballistic Trauma: Lessons Learned from Iraq and Afghanistan

    Science.gov (United States)

    Shin, Emily H.; Sabino, Jennifer M.; Nanos, George P.; Valerio, Ian L.

    2015-01-01

    Management of upper extremity injuries secondary to ballistic and blast trauma can lead to challenging problems for the reconstructive surgeon. Given the recent conflicts in Iraq and Afghanistan, advancements in combat-casualty care, combined with a high-volume experience in the treatment of ballistic injuries, has led to continued advancements in the treatment of the severely injured upper extremity. There are several lessons learned that are translatable to civilian trauma centers and future conflicts. In this article, the authors provide an overview of the physics of ballistic injuries and principles in the management of such injuries through experience gained from military involvement in Iraq and Afghanistan. PMID:25685099

  20. Ballistic transport in graphene grown by chemical vapor deposition

    International Nuclear Information System (INIS)

    In this letter, we report the observation of ballistic transport on micron length scales in graphene synthesised by chemical vapour deposition (CVD). Transport measurements were done on Hall bar geometries in a liquid He cryostat. Using non-local measurements, we show that electrons can be ballistically directed by a magnetic field (transverse magnetic focussing) over length scales of ∼1 μm. Comparison with atomic force microscope measurements suggests a correlation between the absence of wrinkles and the presence of ballistic transport in CVD graphene

  1. Comparative study on sintered alumina for ballistic shielding application

    International Nuclear Information System (INIS)

    This work presents a development of the armor made from special ceramic materials and kevlar. An experimental investigation was conducted to study the ballistic penetration resistance on three samples taken from sintered alumina: a commercial one and two formulations A and B made in IAE/CTA. The main differences between the two formulations was the grain size and bend resistance. The knowledge of the mechanisms during the penetration and perforation process allowed to apply a ductile composite laminate made form kevlar under the alumina to delay its rupture. The last ballistic test showed how a Weibull's modulii and other mechanical properties are able to improve ballistic penetration resistance. (author)

  2. Potential impact of VLSI technologies on guided missile design

    Science.gov (United States)

    Maurer, H. A.; Kongelbeck, K. S.

    1985-08-01

    Some aspects of the anticipated impact of emerging VLSI technologies on tactical missiles, present and future generations are discussed. VLSI evolution represents a unique example of a very dynamic and pervasive trend in commercial and military applications. It is our opinion, however, that the characteristics of this trend are quite different in tactical missiles, not only compared to commercial electronics but even to strategic or space missiles. Considering the particular objectives and constraints as they seem common to most tactical guided missiles and smart munitions, the VLSI technologies should be almost tailored to this application. However, there are some perequisites to be considered to make the introduction of VLSIs successful. Here are some examples: careful planning to be in step with the maturity of the VLSI technology, sensible selection of targets for insertion or new designs and - quite importantly - consideration of program stability in terms of volume, rates, and changes. From a technical viewpoint alone, the current trend to light and small, 4- to 8-inch-diameter configuration whether ground or air-launched encourages an early insertion of VLSIs. Electronic packaging with unusual form factors, e.g., having a central hole for warhead effectiveness, high density and low weight, and low power dissipation, poses conflicting requirements to the missile designer. With very few exceptions, such as in magnetics or battery chemistry, the electronics sections cannot benefit from other technological breakthroughs. It is the evolution of monolithic large scale integration of circuits on Silicon and to a lesser degree on Gallium Arsenide which bears the main load to meeting these criteria of processing density at minimum power dissipation, and of providing an ever-increasing functional throughput. Those VLSI embodiments which appear to be most likely to influence missile electronics are defined. They may be divided into four categories, with some ranking

  3. Ballistic energy transport in PEG oligomers

    Science.gov (United States)

    Lin, Zhiwei; Rubtsova, Natalia I.; Kireev, Victor V.; Rubtsov, Igor V.

    2013-03-01

    Energy transport between the terminal groups of the azido-PEG-succinimide ester compounds with a number of repeating PEG units of 0, 4, 8, and 12 was studied using relaxation-assisted two-dimensional infrared spectroscopy. The through-bond energy transport time, evaluated as the waiting time at which the cross peak maximum is reached, Tmax, was found to be linearly dependent on the chain length for chain lengths up to 60 Å suggesting a ballistic energy transport regime. The through-bond energy transport speed is found to be ca. 500 m/s. The cross-peak amplitude at the maximum decays exponentially with the chain length with a characteristic decay distance of 15.7 ± 1 Å. Substantial mode delocalization across the PEG bridge is found, which can support the energy propagation as a wavepacket.

  4. Ballistic Transport in Graphene Antidot Lattices.

    Science.gov (United States)

    Sandner, Andreas; Preis, Tobias; Schell, Christian; Giudici, Paula; Watanabe, Kenji; Taniguchi, Takashi; Weiss, Dieter; Eroms, Jonathan

    2015-12-01

    The bulk carrier mobility in graphene was shown to be enhanced in graphene-boron nitride heterostructures. However, nanopatterning graphene can add extra damage and drastically degrade the intrinsic properties by edge disorder. Here we show that graphene embedded into a heterostructure with hexagonal boron nitride (hBN) on both sides is protected during a nanopatterning step. In this way, we can prepare graphene-based antidot lattices where the high mobility is preserved. We report magnetotransport experiments in those antidot lattices with lattice periods down to 50 nm. We observe pronounced commensurability features stemming from ballistic orbits around one or several antidots. Due to the short lattice period in our samples, we can also explore the boundary between the classical and the quantum transport regime, as the Fermi wavelength of the electrons approaches the smallest length scale of the artificial potential. PMID:26598218

  5. Ballistics firearm identification by digital holography

    Institute of Scientific and Technical Information of China (English)

    LI Dong-guang

    2009-01-01

    The need for firearm identification systems by police services continues to increase with greater accessibility to weapons in the national and international contexts. The difficulties associated with traditional imaging of ballistics specimens are numerous, and include the smallness of the samples, the nature of the surfaces and shapes for the cartridge cases and projectiles. The digital holography has been introduced to create the 3D image of the fired bullets in order to identify firearms. In digital holography a CCD camera records optically generated holograms which is then reconstructed numerically by a calculation of scalar diffraction in the Fresnel approximation. The digital photography facilitates real time transmission of the message via traditional communication methods. In this paper the principle of digital holography and its application to the 3D image encryption-decryption were reviewed. The experimental results of firearm identification recording using digital holography and their numerical reconstruction were presented.

  6. Real-world ballistics: A dropped bucket

    CERN Document Server

    Hogg, David W

    2007-01-01

    I discuss an apparently simple ballistics problem: the time it takes an object to fall a small vertical distance near the surface of the Earth. It turns out to be not so simple; I spend a great deal of time on the quantitative assessment of the assumptions involved, especially with regards to the influence of the air. The point is \\emph{not} to solve the problem; indeed I don't even end up solving the problem exactly. I introduce dimensional analysis to perform all of the calculations approximately. The principal theme of the lecture is that \\emph{real} physics can be very different from ``textbook'' physics, since in the real world you aren't ever told what equations are appropriate, or why.

  7. Electron Interference in Ballistic Graphene Nanoconstrictions

    Science.gov (United States)

    Baringhaus, Jens; Settnes, Mikkel; Aprojanz, Johannes; Power, Stephen R.; Jauho, Antti-Pekka; Tegenkamp, Christoph

    2016-05-01

    We realize nanometer size constrictions in ballistic graphene nanoribbons grown on sidewalls of SiC mesa structures. The high quality of our devices allows the observation of a number of electronic quantum interference phenomena. The transmissions of Fabry-Perot-like resonances are probed by in situ transport measurements at various temperatures. The energies of the resonances are determined by the size of the constrictions, which can be controlled precisely using STM lithography. The temperature and size dependence of the measured conductances are in quantitative agreement with tight-binding calculations. The fact that these interference effects are visible even at room temperature makes the reported devices attractive as building blocks for future carbon based electronics.

  8. Recognizing plant defense priming

    NARCIS (Netherlands)

    Martinez-Medina, A.; Flors, V.; Heil, M.; Mauch-Mani, B.; Pieterse, C.M.J.; Pozo, M.J.; Ton, J.; Van Dam, N.M.; Conrath, U.

    2016-01-01

    Defense priming conditions diverse plant species for the superinduction of defense, often resulting in enhanced pest and disease resistance and abiotic stress tolerance. Here, we propose a guideline that might assist the plant research community in a consistent assessment of defense priming in plant

  9. 巡航导弹航迹规划决策系统研究与开发%Research on Cruise Missile Route Planning Decision System

    Institute of Scientific and Technical Information of China (English)

    高崇; 沙俊明; 刘学; 张瑜

    2011-01-01

    Based on the research on cruise missile mission planning,adopting TF/TA2(Terrain Following / Terrain Avoiding / Threat Avoiding) technology,the air defense system blind spot caused by earth curvature and topography is using to make missile complete very-low altitude penetration flight for penetration.Cruise missile route planning decision system is designed,including terrain modeling,track decisions,radar emitter library,fire threat library,and the optimal trajectory algorithm.%在研究巡航导弹任务规划的基础上,采用TF/TA2(Terrain Following/Terrain Avoiding/Threat Avoiding)技术,利用地球曲率和地形起伏而造成的防空体系的盲区,使导弹进行超低空飞行,达到突防目的.并设计了巡航导弹航迹规划决策系统,包括地形模拟、航迹决策、雷达辐射源库、火力威胁库的建立和最优航迹算法研究等.

  10. Design and development of Propulsion System for Antitank Guided Missile

    Directory of Open Access Journals (Sweden)

    T. Mohan Reddy

    1995-07-01

    Full Text Available A Propulsion system is designed and developed for the third generation antitank guided missile (ATGM. It consists of a separate booster and sustainer. Booster is ahead of sustainer, having four nozzles canted to the missile axis. Sustainer discharges through a supersonic blast tube. Low smoke, high energy nitramine propellant for this propulsion system developed by the High Energy Materials Research Laboratory (HEMRL, Pune, has been successfully flight-tested. The booster grain is tube-in-tube configuration with end inhibition and the sustainer grain is of end burning configuration. High strength aluminium alloy, HE-15, is used for rocket motor components. Glass-phenolic composite ablative material is used for thermal protection of motors and high density graphite is used for nozzle throats. The design considerations and approach, including grain configuration, nozzle, and ignitersare briefly discussed. The propulsion system has been extensively tested in static tests and in flights, establishing the satisfactory performance of the system.

  11. Assessment of Containment Structures Against Missile Impact Threats

    Institute of Scientific and Technical Information of China (English)

    LI Q M

    2006-01-01

    In order to ensure the highest safety requirements,nuclear power plant structures (the containment structures,the fuel storages and transportation systems) should be assessed against all possible internal and external impact threats.The internal impact threats include kinetic missiles generated by the failure of high pressure vessels and pipes,the failure of high speed rotating machineries and accidental drops.The external impact threats may come from airborne missiles,aircraft impact,explosion blast and fragments.The impact effects of these threats on concrete and steel structures in a nuclear power plant are discussed.Methods and procedures for the impact assessment of nuclear power plants are introduced.Recent studies on penetration and perforation mechanics as well as progresses on dynamic properties of concrete-like materials are presented to increase the understanding of the impact effects on concrete containment structures.

  12. BTT autopilot design for agile missiles with aerodynamic uncer tainty

    Institute of Scientific and Technical Information of China (English)

    Yueyue Ma; Jie Guo; Shengjing Tang

    2015-01-01

    The approach to the synthesis of autopilot with aerody-namic uncertainty is investigated in order to achieve large maneu-verability of agile missiles. The dynamics of the agile missile with reaction-jet control system (RCS) are presented. Subsequently, the cascade control scheme based on the bank-to-turn (BTT) steering technique is described. To address the aerodynamic un-certainties encountered by the control system, the active distur-bance rejection control (ADRC) method is introduced in the autopi-lot design. Furthermore, a compound control er, using extended state observer (ESO) to online estimate system uncertainties and calculate derivative of command signals, is designed based on dynamic surface control (DSC). Nonlinear simulation results show the feasibility of the proposed approach and validate the robust-ness of the control er with severe unmodeled dynamics.

  13. Study of Subsonic Flow Over a TOW 2B Missile

    Science.gov (United States)

    Goudarzi, Koorosh; Jamali, Mehdi

    2016-01-01

    The objective of this investigation is to study the subsonic flow over a missile. In this paper, a model of TOW 2B missile is studied. Two computational approaches are being explored, namely solutions based on the Reynolds-averaged compressible Navier-Stokes equations and solutions based on the inviscid flow (small disturbance theory). The simulations are performed at the Mach number of 0.6, 0.7, 0.8, 0.9 and 1.0 at four angles of attack of 2, 4, 6 and 8 degree. Results obtained from analytical simulation are compared with numerical data. It is found that lift and drag coefficients would go up by increasing of the angle of attack and the Mach number. Trend of changes of the results that obtained from the small disturbance theory is roughly as same as the numeric solution.

  14. Laser-initiated ordnance for air-to-air missiles

    Science.gov (United States)

    Sumpter, David R.

    1993-01-01

    McDonnell Douglas Missile Systems Company (MDMSC) has developed a laser ignition subsystem (LIS) for air-to-air missile applications. The MDMSC subsystem is designed to activate batteries, unlock fins, and sequence propulsion system events. The subsystem includes Pyro Zirconium Pump (PZP) lasers, mechanical Safe & Arm, fiber-optic distribution system, and optically activated pyrotechnic devices (initiators, detonators, and thermal batteries). The LIS design has incorporated testability features for the laser modules, drive electronics, fiber-optics, and pyrotechnics. Several of the LIS have been fabricated and have supported thermal battery testing, integral rocket ramjet testing, and have been integrated into integral rocket ramjet flight test vehicles as part of the flight control subsystem.

  15. A littoral combat model for land-sea missile engagements

    OpenAIRE

    Mahon, Casey M.

    2007-01-01

    Approved for public release; distribution is unlimited This thesis develops a Littoral Combat Model of interactions between Naval Ships at sea and Anti-Ship Cruise Missile Batteries on land. The Littoral Combat Model seeks to answer the question: Is a modern naval force capable of effectively operating in the dangerous littoral environment? The model is derived from a combination of Hughes' Salvo Model and Lanchester's Equations. Cases are developed using either direct fire or area fire we...

  16. Linear Parameter-Varying Feedforward Control: A Missile Autopilot Design

    OpenAIRE

    Theis, Julian; Pfifer, Harald; Knoblach, Andreas; Saupe, Florian; Werner, Herbert

    2015-01-01

    The feedforward path of an autopilot is designed for the longitudinal dynamics of a tactical missile. A linear parameter-varying model is used to synthesize a self-scheduled control law based on a parameter-dependent Lyapunov function. The controller is evaluated on a nonlinear model of industrial complexity both under nominal conditions and parametric uncertainty. Tracking performance is significantly enhanced while leaving robustness properties of an existing feedback controller unaltered.

  17. Decoupling Control Method Based on Neural Network for Missiles

    Institute of Scientific and Technical Information of China (English)

    ZHAN Li; LUO Xi-shuang; ZHANG Tian-qiao

    2005-01-01

    In order to make the static state feedback nonlinear decoupling control law for a kind of missile to be easy for implementation in practice, an improvement is discussed. The improvement method is to introduce a BP neural network to approximate the decoupling control laws which are designed for different aerodynamic characteristic points, so a new decoupling control law based on BP neural network is produced after the network training. The simulation results on an example illustrate the approach obtained feasible and effective.

  18. Local failure of reinforced concrete under missile impact loading

    International Nuclear Information System (INIS)

    This paper deals with the theoretical modelling of the local response of reinforced concrete to missile impact loading. A computer code, SARCASTIC, has been written to serve as a vehicle for the assessment of specific constitutive models for concrete. The code is described: it is axisymmetric (or two dimensional) and uses an explicit integration, Lagrangian finite difference formulation of the equations of motion. Non linear strain tensors and a mesh rotation correction allow large deflection calculations to be performed. (orig.)

  19. Tornado missile risk analysis. Appendixes: anaytical models and data bases. Final report

    International Nuclear Information System (INIS)

    Mathematical models of the contributing events to the tornado missile hazard at nuclear power plants have been developed in which the major sources of uncertainty have been considered in a probablistic framework. These models have been structured into a sequential event formalism which permits the treatment of both single and multiple missile generation events. A simulation computer code utilizing these models has been developed to obtain estimates of tornado missile event likelihoods. Two case studies have been analyzed: a single unit plant using the current NRC set of missiles and a two unit arrangement using an expanded missile set. Preliminary results suggest that the likelihood of missile strike and that of subsequent plant damage may be acceptably small

  20. Tornado missile risk analysis: probability modeling, simulation methodology, and case studies. Final report

    International Nuclear Information System (INIS)

    Mathematical models of the contributing events to the tornado missile hazard at nuclear power plants have been developed in which the major sources of uncertainty have been considered in a probabilistic framework. These models have been structured into a sequential event formalism which permits the treatment of both single and multiple missile generation events. A simulation computer code utilizing these models has been developed to obtain estimates of tornado missile event likelihoods. Two case studies have been analyzed: a single unit plant using the current NRC set of missiles and a two unit arrangement using an expanded missile set. Preliminary results suggest that the likelihood of missile strike and that of subsequent plant damage may be acceptably small

  1. Conditional probability of the tornado missile impact given a tornado occurrence

    International Nuclear Information System (INIS)

    Using an approach based on statistical mechanics, an expression for the probability of the first missile strike is developed. The expression depends on two generic parameters (injection probability eta(F) and height distribution psi(Z,F)), which are developed in this study, and one plant specific parameter (number of potential missiles N/sub p/). The expression for the joint probability of simultaneous impact of muitiple targets is also developed. This espression is applicable to calculation of the probability of common cause failure due to tornado missiles. It is shown that the probability of the first missile strike can be determined using a uniform missile distribution model. It is also shown that the conditional probability of the second strike, given the first, is underestimated by the uniform model. The probability of the second strike is greatly increased if the missiles are in clusters large enough to cover both targets

  2. Design and Simulation of TF and TA Controller for Missile

    Institute of Scientific and Technical Information of China (English)

    ZHA Xu; GUANG Cheng-qi; CUI Ping-yuan; LIU Yong-cai

    2005-01-01

    A nonlinear terrain following(TF) and terrain avoidance(TA) controller is proposed for missile control systems.Based on classical TF algorithm (adaptive angle method), a new method for TF controller is proposed by using angle of attack. A method of obtaining terrain outline data from digital elevation map (DEM) for TF control is discussed in order to save store space. A TA algorithm is proposed by using bank-to-turn technique. The block control model, which is suitable for backstepping design, is given for nonlinear model of missile. Making full use of the characteristics of the system and combining block control principle and backstepping technique, a robust controller design method is proposed. Uncertainties in every sub-block are allowed, and can be canceled by using the idea of nonlinear damping. It is proved that the state tracking errors are converged to a neighborhood of the origin exponentially. Finally, nonlinear six-degree-of-freedom simulation results for the missile model are presented to demonstrate the effectiveness of the proposed control law.

  3. Missile Guidance Law Design via μ-Synthesis

    Science.gov (United States)

    Ochi, Yoshimasa; Itoh, Kouhei; Kanai, Kimio

    A new design method of a robust guidance law for missiles is presented. It has two features. One is that the guidance law is designed based on the heuristic idea that keeping the line-of-sight angular rate small can make the miss distance small. The other is that a linear robust control method, i.e., the μ-synthesis, is employed. When these are incorporated, uncertainties and disturbances in the homing system can explicitly be taken into account in the design to achieve the control or guidance objective. Specifically, the uncertainties and disturbances considered here include time delays in the missile dynamics, range variation between missile and target, measurement noise of the line-of-sight angular rate, and normal target acceleration. The guidance law obtained by this approach is a 4th order dynamic compensator requiring the line-of-sight angular rate as the only measurement. The miss distance is evaluated through nonlinear simulation. The simulation study shows that the proposed guidance law is generally superior to the proportional navigation guidance law and is also superior or equivalent to the suboptimal guidance law in miss distance.

  4. Studies of medium scale non-axisymmetric aluminium missile impacts

    International Nuclear Information System (INIS)

    VTT Technical Research Centre of Finland has studied medium scale missile impacts against rigid and deformable targets to provide data for the calibration and verification of numerical models of a loading scenario where an aircraft impacts against a nuclear power plant. The testing apparatus provides data for validating these models. Missiles used in most of the tests have been cylindrical aluminium and steel pipes. Recent development in the project is tests with a more structurally complex airplane-like missile. Aircraft fuel is also represented as water. The objective of these tests is to produce an impact loading transient with a changing loading area resembling full scale aircraft impact. The tests are also used to develop and verify models of impact scenarios. The goal is to predict the results of the experiments using a mathematical model and if successful, apply the same methods to other impact scenarios. The assumption is made that if the experimental tests can be simulated with accuracy, the same methodology can be applied to full scale phenomenon

  5. Changing law of launching pitching angular velocity of rotating missile

    Institute of Scientific and Technical Information of China (English)

    Liu Guang; Xu Bin; Jiao Xiaojuan; Zhen Tiesheng

    2014-01-01

    In order to provide accurate launching pitching angular velocity (LPAV) for the exterior trajectory optimization design, multi-flexible body dynamics (MFBD) technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model. The built model is verified with the frequency spectrum analysis. With the flexible body contact theory and nonlinear theory of MFBD technology, the research is conducted on the influence of a series of factors on LPAV, such as launching angle change, clearance between launching canister and missile, thrust change, thrust eccentricity and mass eccentricity, etc. Through this research, some useful values of the key design parameters which are difficult to be measured in physical tests are obtained. Finally, a simplified mathematical model of the changing law of LPAV is presented through fitting virtual test results using the linear regression method and verified by physical flight tests. The research results have important significance for the exterior trajectory optimization design.

  6. Changing law of launching pitching angular velocity of rotating missile

    Directory of Open Access Journals (Sweden)

    Liu Guang

    2014-10-01

    Full Text Available In order to provide accurate launching pitching angular velocity (LPAV for the exterior trajectory optimization design, multi-flexible body dynamics (MFBD technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model. The built model is verified with the frequency spectrum analysis. With the flexible body contact theory and nonlinear theory of MFBD technology, the research is conducted on the influence of a series of factors on LPAV, such as launching angle change, clearance between launching canister and missile, thrust change, thrust eccentricity and mass eccentricity, etc. Through this research, some useful values of the key design parameters which are difficult to be measured in physical tests are obtained. Finally, a simplified mathematical model of the changing law of LPAV is presented through fitting virtual test results using the linear regression method and verified by physical flight tests. The research results have important significance for the exterior trajectory optimization design.

  7. Sub-ballistic behaviour of the Quantum Kicked Rotor

    CERN Document Server

    Romanelli, A; Micenmacher, V; Siri, R

    2006-01-01

    We study the resonances of the quantum kicked rotor subjected to an excitation that follows an aperiodic Fibonacci prescription. In such a case the secondary resonances show a sub-ballistic behaviour like the quantum walk with the same aperiodic prescription for the coin. The principal resonances maintain the well-known ballistic behaviour. Then the parallelism previusly established between the kicked rotor and the generalized quantum walk is retained only with the secondary resonances.

  8. Charge transport and shot noise in ballistic graphene sheet

    OpenAIRE

    Sonin, E. B.

    2008-01-01

    The current and the shot noise in a graphene sheet were analyzed in the ballistic regime for arbitrary voltage drops between leads and the sheet in the limit of infinite aspect ratio of the sheet width to its length, when quantization of transversal wave vectors is not essential. The cases of coherent and incoherent ballistic transport were compared. At high voltages the difference with coherent transport is not essential. But at low voltages conductance and Fano-factor dependences for incohe...

  9. The role of ballistic erosion and sedimentation in lunar stratigraphy

    Science.gov (United States)

    Oberbeck, V. R.

    1975-01-01

    Aspects of base surge transport are considered along with questions regarding the applicability of base surge transport to lunar sedimentation, the ballistic transport of crater and basin ejecta, Copernicus crater ballistics, and the effects of ejecta impact on preexisting lunar ground. An ejecta emplacement model is discussed and attention is given to the structure of the surface of continuous deposits of craters and basins, the thickness of crater and basin deposits, and the characteristics of impact melts.

  10. Statistical analysis of ballistic propagation distance in edge turbulence

    International Nuclear Information System (INIS)

    The nonlinear simulation of resistive ballooning turbulence is performed in tokamak edge geometry. The spatiotemporal autocorrelation is calculated for the gradient of turbulent heat flux. The typical ballistic nature in the correlation plot is introduced by the 'Lagrangian correlation', which has spatial and temporal dependence. Propagation distances of the ballistic pulses of the gradient of turbulent heat flux are quantified and are about four times the characteristic size of the front. (author)

  11. The Second National Ballistics Imaging Comparison (NBIC-2)

    OpenAIRE

    Vorburger, TV; Yen, J; Song, JF; Thompson, RM; Renegar, TB; Zheng, A.; Tong, M; Ols, M

    2015-01-01

    In response to the guidelines issued by the American Society of Crime Laboratory Directors/Laboratory Accreditation Board (ASCLD/LAB-International) to establish traceability and quality assurance in U.S. crime laboratories, NIST and the ATF initiated a joint project, entitled the National Ballistics Imaging Comparison (NBIC). The NBIC project aims to establish a national traceability and quality system for ballistics identifications in crime laboratories utilizing ATF’s National Integrated Ba...

  12. Steering and collimating ballistic electrons with amphoteric refraction

    International Nuclear Information System (INIS)

    We show that amphoteric refraction of ballistic electrons, i.e., positive or negative refraction depending on the incidence angle, occurs at an interface between an isotropic and an anisotropic medium and can be employed to steer and collimate electron beams. The steering angle is determined by the materials’ parameters, but the degree of collimation can be tuned in a significant range by changing the energy of ballistic electrons.

  13. The ballistic Mars hopper: An alternative Mars mobility concept

    OpenAIRE

    Sercel, J. C.; Blandino, J. J.; Wood, K. L.

    1987-01-01

    The ballistic Mars hopper is proposed as an alternative mobility concept for unmanned exploration of the martian surface. In the ballistic Mars hopper concept, oxygen and carbon monoxide produced from the martian atmosphere are used as propellants in a rocket propulsion system for an unmanned vehicle on suborbital trajectories between landing sights separated by distances of up to 1000 km. This mobility concept is seen as uniquely capable of allowing both intensive and extensive exploration o...

  14. Relaxed Stable Stability Technology for an Air-to-air Missile

    Institute of Scientific and Technical Information of China (English)

    GUO Zheng-yu; LIANG Xiao-geng

    2012-01-01

    Relaxed Stable Stability (RSS) in an important part of the active control technology. It is a new way to raise the flying speed, distance and maneuverability of missile. Depth study of RSS technology plays an important role for the new concept missile design. This paper describes the detailed definition of RSS and its advantages, pres- ents the research status and prospects for its application in the design of new missiles.

  15. Autopilot Design Method for the Blended Missile Based on Model Predictive Control

    OpenAIRE

    Baoqing Yang; Yuyu Zhao

    2015-01-01

    This paper develops a novel autopilot design method for blended missiles with aerodynamic control surfaces and lateral jets. Firstly, the nonlinear model of blended missiles is reduced into a piecewise affine (PWA) model according to the aerodynamics properties. Secondly, based on the equivalence between the PWA model and mixed logical dynamical (MLD) model, the MLD model of blended missiles is proposed taking into account the on-off constraints of lateral pulse jets. Thirdly, a hybrid model ...

  16. A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft

    Directory of Open Access Journals (Sweden)

    Sebastian Heimbs

    2015-01-01

    Full Text Available An efficient empirical approach was developed to accurately represent the blast shock wave loading resulting from the launch of a missile from a military aircraft to be used in numerical analyses. Based on experimental test series of missile launches in laboratory environment and from a helicopter, equations were derived to predict the time- and position-dependent overpressure. The method was finally applied and validated in a structural analysis of a helicopter tail boom under missile launch shock wave loading.

  17. A Residual Mass Ballistic Testing Method to Compare Armor Materials or Components (Residual Mass Ballistic Testing Method)

    Energy Technology Data Exchange (ETDEWEB)

    Benjamin Langhorst; Thomas M Lillo; Henry S Chu

    2014-05-01

    A statistics based ballistic test method is presented for use when comparing multiple groups of test articles of unknown relative ballistic perforation resistance. The method is intended to be more efficient than many traditional methods for research and development testing. To establish the validity of the method, it is employed in this study to compare test groups of known relative ballistic performance. Multiple groups of test articles were perforated using consistent projectiles and impact conditions. Test groups were made of rolled homogeneous armor (RHA) plates and differed in thickness. After perforation, each residual projectile was captured behind the target and its mass was measured. The residual masses measured for each test group were analyzed to provide ballistic performance rankings with associated confidence levels. When compared to traditional V50 methods, the residual mass (RM) method was found to require fewer test events and be more tolerant of variations in impact conditions.

  18. Analysis of Temporary Cavity Produced by High Velocity Missile in Gelatin Blocks

    OpenAIRE

    Korać, Želimir; Kelenc, Dubravko; Mikulić, Danko; Hančević, Janko

    2000-01-01

    The effects of high velocity missiles (a Russian AK-74 assault rifle, 5.45 mm) in a tissue simulant • gelatin block were analyzed. The characteristics of temporary cavity were studied by the analysis of calibrated images of the missile path. The missile path through the block was visualized using a TV camera with an ultra-speed shutter. TV picture was calibrated before the shooting. Cross-section of the temporary cavity was measured as a function of distance from the missile entry point. The ...

  19. Dynamics and thermal sensitivity of ballistic and non-ballistic feeding in salamanders.

    Science.gov (United States)

    Deban, Stephen M; Scales, Jeffrey A

    2016-02-01

    Low temperature reduces the performance of muscle-powered movements, but in movements powered by elastic recoil mechanisms, this effect can be mitigated and performance can be increased. To better understand the morphological basis of high performance and thermal robustness of elastically powered movements, we compared feeding dynamics at a range of temperatures (5-25°C) in two species of terrestrial plethodontid salamanders, Plethodon metcalfi and Ensatina eschscholtzii, which differ in tongue muscle architecture and the mechanism of tongue projection. We found that Ensatina is capable of ballistic projection with a mean muscle mass-specific power of 2100 W kg(-1), revealing an elastic mechanism. Plethodon, in contrast, projected its tongue non-ballistically with a mean power of only 18 W kg(-1), indicating it is muscle powered. Ensatina projected its tongue significantly farther than Plethodon and with dynamics that had significantly lower thermal sensitivity at temperatures below 15°C. These performance differences were correlated with morphological differences, namely elongated collagenous aponeuroses in the projector muscle of Ensatina as compared with Plethodon, which are likely the site of energy storage, and the absence in Ensatina of projector muscle fibers attaching to the tongue skeleton that allows projection to be truly ballistic. These findings demonstrate that, in these otherwise similar species, the presence in one species of elaborated connective tissue in series with myofibers confers not only 10-fold greater absolute performance but also greater thermal robustness of performance. We conclude that changes in muscle and connective tissue architecture are sufficient to alter significantly the mechanics, performance and thermal robustness of musculoskeletal systems.

  20. Moving Target Defense

    CERN Document Server

    Jajodia, Sushil; Swarup, Vipin; Wang, Cliff; Wang, X Sean

    2011-01-01

    Moving Target Defense: Creating Asymmetric Uncertainty for Cyber Threats was developed by a group of leading researchers. It describes the fundamental challenges facing the research community and identifies new promising solution paths. Moving Target Defense which is motivated by the asymmetric costs borne by cyber defenders takes an advantage afforded to attackers and reverses it to advantage defenders. Moving Target Defense is enabled by technical trends in recent years, including virtualization and workload migration on commodity systems, widespread and redundant network connectivity, instr

  1. Takeover Defenses and Competition

    OpenAIRE

    Martijn Cremers; Vinay Nair; Urs Peyer

    2007-01-01

    This paper studies the interaction between takeover defenses and product market competition. We find that firms in more competitive industries have more takeover defenses. This is the opposite result from what one would expect if takeover defenses always constitute an inefficient outcome that increases agency costs and managerial entrenchment. A novel explantion is provided by considering the nature of the relationship between the firm and the product (or labor) market. For firms in industrie...

  2. Norwegian cyber defense

    OpenAIRE

    Stensboel, Karl Birger

    2013-01-01

    Approved for public release; distribution is unlimited. This thesis postulates the need for a more proactive approach to cyber defense in Norway and offers recommendations about how Norway can be better prepared to counter cyber threats. It finds that Norways strategic infrastructure is vulnerable to cyber attacks and that Norway has no coherent strategy for meeting this challenge. The thesis argues that an effective cyber defense requires a wide range of offensive and defensive measures a...

  3. [Bullet and shrapnel injuries in the face and neck regions. Current aspects of wound ballistics].

    Science.gov (United States)

    Hauer, T; Huschitt, N; Kulla, M; Kneubuehl, B; Willy, C

    2011-08-01

    A basic understanding of the ballistic behaviour of projectiles or fragments after entering the human body is essential for the head and neck surgeon in the military environment in order to anticipate the diagnostic and therapeutic consequences of this type of injury. Although a large number of factors influence the missile in flight and after penetration of the body, the most important factor is the amount of energy transmitted to the tissue. Long guns (rifles or shotguns) have a much higher muzzle energy compared to handguns, explaining why the remote effects beyond the bullet track play a major role. While most full metal jacket bullets release their energy after 12-20 cm (depending on the calibre), soft point bullets release their energy immediately after entry into the human body. This results in a major difference in extremity wounds, but not so much in injuries with long bullet paths (e.g. diagonal shots). Shrapnel wounds are usually produced with similarly high kinetic energy to those caused by hand- and long guns. However, fragments tend to dissipate the entire amount of energy within the body, which increases the degree of tissue disruption. Of all relevant injuries in the head and neck region, soft tissue injuries make up the largest proportion (60%), while injuries to the face are seen three times more often than injuries to the neck. Concomitant intracranial or spinal injury is seen in 30% of cases. Due to high levels of wound contamination, the infection rate is approximately 15%, often associated with a complicated and/or multiresistant spectrum of germs. PMID:21833833

  4. Superconducting Graphene Nanodevices in Ballistic Transport Regime

    Science.gov (United States)

    Chen, Yu-An; Wang, Joel I.-Jan; Watanabe, Kenji; Taniguchi, Takashi; Jarillo-Herrero, Pablo; Pablo Jarillo-Herrero's Group Team

    2013-03-01

    Superconductivity carried by Dirac fermions can be realized through induced superconductivity in grapheme. Observation of novel phenomena anticipated by theories requires graphene devices with low disorder whereas the carrier transport is ballistic. Current fabrication procedures to make graphene devices with low disorder like suspension or ultra-flat substrates all call for certain kinds of annealing to remove organic residues derived from the fabrication process. Applying these methods to superconducting devices can be challenging since the transparency at the graphene/superconductor interface will be destroyed. Here we present a method to do dry transfer of patterned hexagonal Boron Nitride (hBN) flakes onto graphene. The ultra flatness and lack of dangling bond in the boron nitride substrate reduces the disorder in graphene, and the top layer hBN can protect the graphene from contamination in the nanofabrication procedures and yield the geometry desired for different experimental exploration. National Institute for Materials Science, Namiki 1-1, Tsukuba, Ibaraki 305-0044, Japan

  5. Dynamic defense workshop :

    Energy Technology Data Exchange (ETDEWEB)

    Crosby, Sean Michael; Doak, Justin E.; Haas, Jason Juedes.; Helinski, Ryan; Lamb, Christopher C.

    2013-02-01

    On September 5th and 6th, 2012, the Dynamic Defense Workshop: From Research to Practice brought together researchers from academia, industry, and Sandia with the goals of increasing collaboration between Sandia National Laboratories and external organizations, de ning and un- derstanding dynamic, or moving target, defense concepts and directions, and gaining a greater understanding of the state of the art for dynamic defense. Through the workshop, we broadened and re ned our de nition and understanding, identi ed new approaches to inherent challenges, and de ned principles of dynamic defense. Half of the workshop was devoted to presentations of current state-of-the-art work. Presentation topics included areas such as the failure of current defenses, threats, techniques, goals of dynamic defense, theory, foundations of dynamic defense, future directions and open research questions related to dynamic defense. The remainder of the workshop was discussion, which was broken down into sessions on de ning challenges, applications to host or mobile environments, applications to enterprise network environments, exploring research and operational taxonomies, and determining how to apply scienti c rigor to and investigating the eld of dynamic defense.

  6. Defense Mechanisms: A Bibliography.

    Science.gov (United States)

    Pedrini, D. T.; Pedrini, Bonnie C.

    This bibliography includes studies of defense mechanisms, in general, and studies of multiple mechanisms. Defense mechanisms, briefly and simply defined, are the unconscious ego defendants against unpleasure, threat, or anxiety. Sigmund Freud deserves the clinical credit for studying many mechanisms and introducing them in professional literature.…

  7. Forgiveness and Defense Style

    Science.gov (United States)

    Maltby, John; Day, Liz

    2004-01-01

    Within the literature on the psychology of forgiveness, researchers have hypothesized that the 1st stage in the process of being able to forgive is the role of psychological defense. To examine such a hypothesis, the authors explored the relationship between forgiveness and defense style. The 304 respondents (151 men, 153 women) completed measures…

  8. Transition to ballistic regime for heat transport in helium II

    Energy Technology Data Exchange (ETDEWEB)

    Sciacca, Michele, E-mail: michele.sciacca@unipa.it [Dipartimento Scienze Agrarie e Forestali, Università degli studi di Palermo, Viale delle Scienze, 90128 Palermo (Italy); Departament de Física, Universitat Autònoma de Barcelona, 08193 Bellaterra, Catalonia (Spain); Sellitto, Antonio, E-mail: ant.sellitto@gmail.com [Dipartimento di Matematica, Informatica ed Economia, Università della Basilicata, Campus Macchia Romana, 85100 Potenza (Italy); Jou, David, E-mail: david.jou@uab.cat [Departament de Física, Universitat Autònoma de Barcelona, 08193 Bellaterra, Catalonia (Spain); Institut d' Estudis Catalans, Carme 47, 08001 Barcelona, Catalonia (Spain)

    2014-07-04

    The size-dependent and flux-dependent effective thermal conductivity of narrow capillaries filled with superfluid helium is analyzed from a thermodynamic continuum perspective. The classical Landau evaluation of the effective thermal conductivity of quiescent superfluid, or the Gorter–Mellinck regime of turbulent superfluids, is extended to describe the transition to ballistic regime in narrow channels wherein the radius R is comparable to (or smaller than) the phonon mean-free path ℓ in superfluid helium. To do so, we start from an extended equation for the heat flux incorporating non-local terms, and take into consideration a heat slip flow along the walls of the tube. This leads from an effective thermal conductivity proportional to R{sup 2} (Landau regime) to another one proportional to Rℓ (ballistic regime). We consider two kinds of flows: along cylindrical pipes and along two infinite parallel plates. - Highlights: • Heat transport in counterflow helium in the ballistic regime. • The one-fluid model based on the Extended Thermodynamics is used. • The transition from the Landau regime to the ballistic regime. • The transition from quantum turbulence to ballistic regime.

  9. Improvement of Interior Ballistic Performance Utilizing Particle Swarm Optimization

    Directory of Open Access Journals (Sweden)

    Hazem El Sadek

    2014-01-01

    Full Text Available This paper investigates the interior ballistic propelling charge design using the optimization methods to select the optimum charge design and to improve the interior ballistic performance. The propelling charge consists of a mixture propellant of seven-perforated granular propellant and one-hole tubular propellant. The genetic algorithms and some other evolutionary algorithms have complex evolution operators such as crossover, mutation, encoding, and decoding. These evolution operators have a bad performance represented in convergence speed and accuracy of the solution. Hence, the particle swarm optimization technique is developed. It is carried out in conjunction with interior ballistic lumped-parameter model with the mixture propellant. This technique is applied to both single-objective and multiobjective problems. In the single-objective problem, the optimization results are compared with genetic algorithm and the experimental results. The particle swarm optimization introduces a better performance of solution quality and convergence speed. In the multiobjective problem, the feasible region provides a set of available choices to the charge’s designer. Hence, a linear analysis method is adopted to give an appropriate set of the weight coefficients for the objective functions. The results of particle swarm optimization improved the interior ballistic performance and provided a modern direction for interior ballistic propelling charge design of guided projectile.

  10. Transition to ballistic regime for heat transport in helium II

    International Nuclear Information System (INIS)

    The size-dependent and flux-dependent effective thermal conductivity of narrow capillaries filled with superfluid helium is analyzed from a thermodynamic continuum perspective. The classical Landau evaluation of the effective thermal conductivity of quiescent superfluid, or the Gorter–Mellinck regime of turbulent superfluids, is extended to describe the transition to ballistic regime in narrow channels wherein the radius R is comparable to (or smaller than) the phonon mean-free path ℓ in superfluid helium. To do so, we start from an extended equation for the heat flux incorporating non-local terms, and take into consideration a heat slip flow along the walls of the tube. This leads from an effective thermal conductivity proportional to R2 (Landau regime) to another one proportional to Rℓ (ballistic regime). We consider two kinds of flows: along cylindrical pipes and along two infinite parallel plates. - Highlights: • Heat transport in counterflow helium in the ballistic regime. • The one-fluid model based on the Extended Thermodynamics is used. • The transition from the Landau regime to the ballistic regime. • The transition from quantum turbulence to ballistic regime

  11. Ballistic heat conduction and mass disorder in one dimension

    International Nuclear Information System (INIS)

    It is well-known that in the disordered harmonic chain, heat conduction is subballistic and the thermal conductivity (κ) scales asymptotically as limL→∞κ∝L0.5 where L is the chain length. However, using the nonequilibrium Green's function (NEGF) method and analytical modelling, we show that there exists a critical crossover length scale (LC) below which ballistic heat conduction (κ∝L) can coexist with mass disorder. This ballistic-to-subballistic heat conduction crossover is connected to the exponential attenuation of the phonon transmittance function Ξ i.e. Ξ(ω, L) = exp[−L/λ(ω)], where λ is the frequency-dependent attenuation length. The crossover length can be determined from the minimum attenuation length, which depends on the maximum transmitted frequency. We numerically determine the dependence of the transmittance on frequency and mass composition as well as derive a closed form estimate, which agrees closely with the numerical results. For the length-dependent thermal conductance, we also derive a closed form expression which agrees closely with numerical results and reproduces the ballistic to subballistic thermal conduction crossover. This allows us to characterize the crossover in terms of changes in the length, mass composition and temperature dependence, and also to determine the conditions under which heat conduction enters the ballistic regime. We describe how the mass composition can be modified to increase ballistic heat conduction. (paper)

  12. Opportunities and challenges for MEMS technology in Army missile systems applications

    Science.gov (United States)

    Ruffin, Paul B.

    1999-07-01

    The military market drives the thrust for the development of robust, high performance MicroElectroMechanical Systems (MEMS) devices with applications such as: competent and smart munitions, aircraft and missile autopilots, tactical missile guidance, fire control systems, platform stabilization, smart structures with embedded inertial sensors, missile system health monitoring, aerodynamic flow control, and multiple intelligent small projectiles. Army missile applications will be a fertile market for MEMS products, such as MEMS-based inertial sensors. MEMS technology should significantly enhance performance and provide more robust mission capability in applications where arrays of MEMS devices are required. The Army Aviation and Missile Command Missile Research, Development, and Engineering Center is working diligently with other government agencies, academia, and industry to develop high performing MEMS devices to withstand shock, vibration, temperature, humidity, and long-term storage conditions often encountered by Army missile systems. The goals of the ongoing DARPA MEMS technology programs will meet a significant portion of the Army missile systems requirements. In lieu of presenting an all-inclusive review of Army MEMS applications, this paper addresses a number of opportunities and associated challenges for MEMS systems operating in military environments. Near term applications and the less mature, high-risk applications of MEMS devices are addressed.

  13. 78 FR 48503 - Proposed Revision to Missiles Generated by Extreme Winds

    Science.gov (United States)

    2013-08-08

    ... COMMISSION Proposed Revision to Missiles Generated by Extreme Winds AGENCY: Nuclear Regulatory Commission....4, ``Missiles Generated by Extreme Winds,'' of NUREG-0800, ``Standard Review Plan for the Review of... extreme winds. The revision also incorporates guidance on regulatory treatment of nonsafety systems....

  14. Laser active imaging-guided anti-tank missile system small-scale integration design

    Science.gov (United States)

    Yan, Mingliang; Shan, Xiangqian; Qu, Zhou

    2010-10-01

    At present, the domestic and international third-generation anti-tank missiles, laser-guided missiles are mostly divided into active laser-guided and laser semi-active guidance, this guidance system, there are vulnerable to electronic interference, can not be fully realized after launching deficiencies. Article based on this, an in-depth understanding of imaging-guided laser-active working principle, based on the pairs of third-generation anti-tank missile guidance system, boldly proposed to improve the anti-tank missiles, laser-active small-scale integration of imaging guidance system design, the main purpose is to improve a certain type of The optical target missile, TV angle measurement, laser-guided instruction transmission means, so that anti-tank missiles to achieve forward-looking, the next obstacle avoidance TV and multi-functional integration of the entire after launching smart missiles, and in theory be able to study the new antitank missiles play a certain reference.

  15. A modular ducted rocket missile model for threat and performance assessment

    NARCIS (Netherlands)

    Mayer, A.E.H.J.; Halswijk, W.H.C.; Komduur, H.J.; Lauzon, M.; Stowe, R.A.

    2005-01-01

    A model was developed to predict the thrust of throttled ramjet propelled missiles. The model is called DRCORE and fulfils the growing need to predict the performance of air breathing missiles. Each subsystem of the propulsion unit of this model is coded by using engineering formulae and enables the

  16. Study on the perforation of reinforced concrete slabs by rigid missiles. General introduction

    International Nuclear Information System (INIS)

    Problems encountered in computing nuclear plant protective devices against the impact of a given rigid missile (e.g. turbine disc fragments) are emphasized. The experimental program of balistic tests (missile velocities between 90m.s-1 and 170m.s-2) and reduced scale tests carried out in France is briefly outlined

  17. Missile Sites, Former missile field for Whiteman., Published in 2005, 1:12000 (1in=1000ft) scale, Whiteman Air Force Base.

    Data.gov (United States)

    NSGIC GIS Inventory (aka Ramona) — This Missile Sites dataset, published at 1:12000 (1in=1000ft) scale, was produced all or in part from Field Survey/GPS information as of 2005. It is described as...

  18. Launch Stabilisation System for Vertical Launch of a Missile

    Directory of Open Access Journals (Sweden)

    K. Sreekumar

    2005-07-01

    Full Text Available The launch platform stabilisation control system is a roll-pitch stabilised platform for the vertical launch of a missile from a naval ship. Stabilisation of the launch platform is achievedwith the help of embedded controllers and electro-hydraulic servo control system. The launch platform is stabilised wrt true horizontal with a 2-axis (roll and pitch stabilisation systemconsisting of a gimbal and a set of three high-pressure servo hydraulic actuators. The control system uses rate gyro and tilt sensor feedbacks for stabilising the platform. This paper outlines the details of the launch platform stabilisation control system, results of digital simulation, and the performance during sea trials.

  19. The Eastern Space and Missile Center - Jonathan Dickinson Instrumentation Facility

    Science.gov (United States)

    Beckner, H. E.; Clark, S. R.; Bonner, J. R.; Thomas, C. G.

    The Jonathan Dickinson Instrumentation Facility (JDIF) is an instrumentation station at the Eastern Test Range designed to provide space diversity tracking of all launches from the Eastern Space and Missile Center or Kennedy Space Center. The JDIF includes tracking radar, telemetry, command/control systems, timing, and communication systems and the Navy's Flight Test Support System in one integrated building. Since virtually all of the instrumentation at JDIF is critical to the success of launches, a concept was established to make it possible to run the Eastern Test Range site during mission support from a bank of diesel generators, and to use commercial power for normal day-to-day operations.

  20. Renewable Energy Opportunities at White Sands Missile Range, New Mexico

    Energy Technology Data Exchange (ETDEWEB)

    Chvala, William D.; Solana, Amy E.; States, Jennifer C.; Warwick, William M.; Weimar, Mark R.; Dixon, Douglas R.

    2008-09-01

    The document provides an overview of renewable resource potential at White Sands Missile Range (WSMR) based primarily upon analysis of secondary data sources supplemented with limited on-site evaluations. The effort was funded by the U.S. Army Installation Management Command (IMCOM) as follow-on to the 2005 DoD Renewable Energy Assessment. This effort focuses on grid-connected generation of electricity from renewable energy sources and also ground source heat pumps (GSHPs) for heating and cooling buildings, as directed by IMCOM.

  1. Computer aided design and manufacturing of composite propfan blades for a cruise missile wind tunnel model

    Science.gov (United States)

    Thorp, Scott A.; Downey, Kevin M.

    1992-01-01

    One of the propulsion concepts being investigated for future cruise missiles is advanced unducted propfans. To support the evaluation of this technology applied to the cruise missile, a joint DOD and NASA test project was conducted to design and then test the characteristics of the propfans on a 0.55-scale, cruise missile model in a NASA wind tunnel. The configuration selected for study is a counterrotating rearward swept propfan. The forward blade row, having six blades, rotates in a counterclockwise direction, and the aft blade row, having six blades, rotates in a clockwise direction, as viewed from aft of the test model. Figures show the overall cruise missile and propfan blade configurations. The objective of this test was to evaluate propfan performance and suitability as a viable propulsion option for next generation of cruise missiles. This paper details the concurrent computer aided design, engineering, and manufacturing of the carbon fiber/epoxy propfan blades as the NASA Lewis Research Center.

  2. Simulation Analysis of Wave Effect on Exceeding Water Gesture and Load of Submarine Launched Missile

    Directory of Open Access Journals (Sweden)

    Ke Zhao

    2014-02-01

    Full Text Available In this study, we have a research on wave action on the submarine launched missile water trajectory and gesture angles during the process between launch and exit from water. Infinite water depth plane wave was used as the wave model, mathematics models of missile exceeding water under different wave conditions were established based on ideal potential flow theory. The flow field velocity potential was obtained by solving the Laplace equation, thus can obtain missile surface pressure. Considering free surface effects, simple Green’s function was introduced to solve boundary value problems. Three-dimensional Fortran program and finite software ABAQUS were combined to complete the fluid-structure interaction simulation. The rules that wave level and phases effects on submarine-launched missile were finally obtained, which shows wave affect cannot be neglected. Simulation methods and results of this study have a certain reference value for the submarine-launched missile launching.

  3. Local impact effects on concrete target due to missile: An empirical and numerical approach

    International Nuclear Information System (INIS)

    Highlights: • Local impact effect of hard missile on reinforced concrete targets has been studied. • Review of empirical formulation for predicting local response carried out. • Numerical simulation of experimental test of Kojima (1991) carried out. • Divergence of FE results with those obtained using emperical formulations. • Close match of numerical simulation results with experimental data. - Abstract: Concrete containment walls and internal concrete barrier walls of a Nuclear Power Plant safety related structures are often required to be designed for externally and internally generated missiles. Potential missiles include external extreme wind generated missiles, aircraft crash and internal accident generated missiles such as impact due to turbine blade failure and steel pipe missiles resulting from pipe break. The objective of the present paper is to compare local missile impact effects on reinforced concrete target using available empirical formulations with those obtained using LS-DYNA numerical simulation. The use of numerical simulations for capturing the transient structural response has become increasingly used for structural design against impact loads. They overcome the limits of applicability of the empirical formulae and also provide information on stress and deformation fields, which may be used to improve the resistance of the concrete. Finite element (FE) analyses of an experimental impact problem reported by Kojima (1991) are carried out that are able to capture the missile impact effects; in terms of local and global damage. The continuous surface cap model has been used for modelling concrete behaviour. A range of missile velocity has been considered to simulate local missile impact phenomenon and modes of failure and to capture the concrete response from elastic to plastic fracture. A comparison is then made between the empirical formulations, numerical simulation results, and available experimental results of slab impact tests

  4. Relationship between Ballistic Coefficient and Static Mechanical Properties for Armor Materials

    Institute of Scientific and Technical Information of China (English)

    2001-01-01

    The relationship between the ballistic coefficient and the static mechanical properties of armor materials was studied. The results show that the ballistic coefficient is determined by the strength, hardness and the toughness of materials. According to the Martel rule, the equation of the relationship between ballistic coefficient and static mechanical properties satisfies the following formula: . From the mixture law of composite, the prerequisite, for which ballistic coefficient has maximum to reinforcement volume fraction, is obtained by the following equation: .

  5. ["Piggyback" shot: ballistic parameters of two simultaneously discharged airgun pellets].

    Science.gov (United States)

    Frank, Matthias; Schönekess, Holger C; Grossjohann, Rico; Ekkernkamp, Axel; Bockholdt, Britta

    2014-01-01

    Green and Good reported an uncommon case of homicide committed with an air rifle in 1982 (Am. J. Forensic Med. Pathol. 3: 361-365). The fatal wound was unusual in that two airgun pellets were loaded in so-called "piggyback" fashion into a single shot air rifle. Lack of further information on the ballistic characteristics of two airgun pellets as opposed to one conventionally loaded projectile led to this investigation. The mean kinetic energy (E) of the two pellets discharged in "piggyback" fashion was E = 3.6 J and E = 3.4 J, respectively. In comparison, average kinetic energy values of E = 12.5 J were calculated for conventionally discharged single diabolo pellets. Test shots into ballistic soap confirmed the findings of a single entrance wound as reported by Green and Good. While the ballistic background of pellets discharged in "piggyback" fashion could be clarified, the reason behind this mode of shooting remains unclear. PMID:24855739

  6. Ballistic spin filtering across the ferromagnetic-semiconductor interface

    Directory of Open Access Journals (Sweden)

    Y.H. Li

    2012-03-01

    Full Text Available The ballistic spin-filter effect from a ferromagnetic metal into a semiconductor has theoretically been studied with an intention of detecting the spin polarizability of density of states in FM layer at a higher energy level. The physical model for the ballistic spin filtering across the interface between ferromagnetic metals and semiconductor superlattice is developed by exciting the spin polarized electrons into n-type AlAs/GaAs superlattice layer at a much higher energy level and then ballistically tunneling through the barrier into the ferromagnetic film. Since both the helicity-modulated and static photocurrent responses are experimentally measurable quantities, the physical quantity of interest, the relative asymmetry of spin-polarized tunneling conductance, could be extracted experimentally in a more straightforward way, as compared with previous models. The present physical model serves guidance for studying spin detection with advanced performance in the future.

  7. Quantum Point Contact Transistor and Ballistic Field-Effect Transistors

    International Nuclear Information System (INIS)

    We report the experimental results and theoretical understanding of the Quantum Point Contact Transistor - a fully ballistic one-dimensional (1D) Field-Effect Transistor (FET). Experimentally obtained voltage gain greater than 1 in our Quantum-Point-Contact transistors at 4.2 K can be explained with the help of an analytical modeling based on the Landauer-Büttiker approach in mesosopic physics: the lowest 1D subband and the band gap play the key role in increasing its transconductance, especially by reducing its output conductance, and thus achieving a voltage gain higher than 1. This work provides a general basis for devising future ballistic FETs and the quantum limits found in this work may be used to estimate normalized transconductance and channel resistance in future two-dimensional (2D) ballistic FETs.

  8. Ballistic-neutralized chamber transport of intense heavy ion beams

    International Nuclear Information System (INIS)

    Two-dimensional particle-in-cell simulations of intense heavy ion beams propagating in an inertial confinement fusion (ICF) reactor chamber are presented. The ballistic-neutralized transport scheme studied uses 4 GeV Pb+1 ion beams injected into a low-density, gas-filled reactor chamber and the beam is ballistically focused onto an ICF target before entering the chamber. Charge and current neutralization of the beam is provided by the low-density background gas. The ballistic-neutralized simulations include stripping of the beam ions as the beam traverses the chamber as well as ionization of the background plasma. In addition, a series of simulations are presented that explore the charge and current neutralization of the ion beam in an evacuated chamber. For this vacuum transport mode, neutralizing electrons are only drawn from sources near the chamber entrance

  9. Development of high-density ceramic composites for ballistic applications

    International Nuclear Information System (INIS)

    The application of ceramic composites for ballistic application has been generally developed with ceramics of low density, between 2.5 and 4.5 g/cm2. These materials have offered good performance in defeating small-caliber penetrators, but can suffer time-dependent degradation effects when thicker ceramic tiles are needed to defeat modem, longer, heavy metal penetrators that erode rather than break up. This paper addresses the ongoing development, fabrication procedures, analysis, and ballistic evaluation of thinner, denser ceramics for use in armor applications. Nuclear Metals Incorporated (NMI) developed a process for the manufacture of depleted uranium (DU) ceramics. Samples of the ceramics have been supplied to the US Army Research Laboratory (ARL) as part of an unfunded cooperative study agreement. The fabrication processes used, characterization of the ceramic, and a ballistic comparison between the DU-based ceramic with baseline Al2O3 will be presented

  10. Defense Industry Clusters in Turkey

    Directory of Open Access Journals (Sweden)

    Kadir Alpaslan Demir

    2016-06-01

    Full Text Available All countries strive for a capable national defense supported by a strong national defense industry. Supporting national defense with imported defense systems has many limitations and risks because the terms of arms trade agreements between countries may easily be influenced by the political climate of the signatories. As a result, establishing an independent national defense requires a strong national defense industry. Furthermore, exporting defense systems may be an important source of national income. National defense industries mostly consist of large-scale defense firms that have the resources required for big defense contracts. However, small to medium enterprises (SMEs do not have the necessary resources, therefore they are at a disadvantage. To overcome this handicap and be part of the business, defense industry clusters mostly consisting of SMEs are being established. Provided that there is good national planning and support in this area, defense clusters consisting of SMEs may play a significant role in industry. SMEs have a chance to offer specialized services, special or customized products when needed. As a result, large defense firms subcontract certain portions of defense projects to SMEs. Since 2010, Turkey has shown signs of continuous improvement in defense industry clustering. In parallel with these developments, this study discusses the importance of clustering in the defense industry, briefly presents the state of the Turkish defense industry as highlighted by national statistics, and presents the current status of defense clusters in Turkey. The novelty of this article consists in its assessment of Turkish defense clusters.

  11. Operating process optimization in a ballistic plasmatron with multistage heating

    International Nuclear Information System (INIS)

    The study on operating modes of ballistic plasmatrons is carried out. Optimization parameters and operating modes of these devices made it possible to increase by 10-20 times their efficiency. The energy characteristics achieved as well as self-regulation and high coefficient of the pushing gas energy conversion into the plasma emission energy in the optical and ultraviolet wave ranges (up to 30% in real experimental devices) enable the extension of the application area of the sources of the optical and ultraviolet radiation on the basis of ballistic plasmatrons

  12. Ballistic bunching theory of electron cyclotron resonance masers

    Energy Technology Data Exchange (ETDEWEB)

    Baik, C. W.; Jeon, S. G.; Park, G. S. [Seoul National University, Seoul (Korea, Republic of)

    2003-12-15

    A bunching parameter which determines the strength of modulation in electron cyclotron resonance masers (ECRM) is derived using a ballistic bunching theory. Unlike klystrons that utilize space bunching, this bunching parameter strongly depends on the beam velocity ratio due to phase bunching in ECRM. The dependencies of the beam velocity ratio ({approx} {alpha}{sup 2}), the interaction length ({approx} d), and the input drive power ({approx} P{sub in}{sup 1/2}) on the bunching parameter are derived. The orbital phase bunching results calculated using the ballistic bunching theory and a large-signal code are compared and show reasonable agreement.

  13. Gunshot wounds: A review of ballistics related to penetrating trauma

    Directory of Open Access Journals (Sweden)

    Panagiotis K. Stefanopoulos

    2014-01-01

    Full Text Available Civilian gunshot injuries from handgun and rifle ammunition vary in severity depending on the anatomic location involved and the different effects from the ballistic properties of the penetrating projectiles. Ballistic factors such as the impact velocity and energy should not be considered in isolation, as their specific effects are determined by the interaction between the projectile and tissues. Increased tissue damage can result from tumbling of non-deforming rifle bullets and deformation of expanding bullets. Both of these mechanisms increase substantially the energy transfer to the wound and its diameter, also producing a pulsating temporary cavity associated with pressure changes within tissue.

  14. Ballistics for neurosurgeons: Effects of firearms of customized cranioplasty implants

    OpenAIRE

    Lemcke, Johannes; Löser, Rainer; Telm, Andreas; Meier, Ullrich; Hunt, C. David

    2013-01-01

    Introduction: There are about 33,000 deaths caused by gunshot wounds in the USA each year. Probably half of these deaths result from head wounds. Among US Army soldiers, 17% of all ballistic injuries are head wounds. This means that, even in those protected by ballistic helmets, gunshot injuries to the head represent a danger. The aim of this study was to examine the effects of shelling of computer-aided designed (CAD) cranioplasty implants made of two different materials. Methods: An experim...

  15. Low-Energy Ballistic Transfers to Lunar Halo Orbits

    Science.gov (United States)

    Parker, Jeffrey S.

    2009-01-01

    Recent lunar missions have begun to take advantage of the benefits of low-energy ballistic transfers between the Earth and the Moon rather than implementing conventional Hohmann-like lunar transfers. Both Artemis and GRAIL plan to implement low-energy lunar transfers in the next few years. This paper explores the characteristics and potential applications of many different families of low-energy ballistic lunar transfers. The transfers presented here begin from a wide variety of different orbits at the Earth and follow several different distinct pathways to the Moon. This paper characterizes these pathways to identify desirable low-energy lunar transfers for future lunar missions.

  16. Ballistic thermoelectric properties in double-bend graphene nanoribbons

    International Nuclear Information System (INIS)

    Ballistic thermoelectric properties in double-bend graphene nanoribbons (GNRs) are investigated by using the nonequilibrium Green's function. We find that due to the elastic scattering caused by the interface mismatching, the thermal conductance contributed by phonons is greatly reduced, while ballistic transport behaviors for electrons are dramatically demolished, and even some gaps can be opened at antiresonance energies. Near these antiresonance gaps, the maximum value of ZT (ZTmax) can be observed, much larger than that for straight GNRs. Moreover, this ZTmax can be effectively tuned by modulating the length or width of double-bend GNRs.

  17. A microscopic model of ballistic-diffusive crossover

    International Nuclear Information System (INIS)

    Several low-dimensional systems show a crossover from diffusive to ballistic heat transport when system size is decreased. Although there is some phenomenological understanding of this crossover phenomenon at the coarse-grained level, a microscopic picture that consistently describes both the ballistic and the diffusive transport regimes has been lacking. In this work we derive a scaling form for the thermal current in a class of one dimensional systems attached to heat baths at boundaries and rigorously show that the crossover occurs when the characteristic length scale of the system competes with the system size. (paper)

  18. Internal Ballistics of High Velocity Special Purpose Guns

    Directory of Open Access Journals (Sweden)

    V. K. Gupta

    1976-07-01

    Full Text Available More and more conventional guns are being utilized as special purpose guns to achieve very high velocity by using unconventionally high C/W ratios. The existing methods of internal ballistics give satisfactory results only for low (less than one C/W ratios. In the present paper the basic internal ballistic equations have been modified to cater for non-linear rate of burning, cubical form function and a realistic pressure gradient between breech face and the projectile base. The equations have been numerically solved. The results for low and high C/W ratios have been compared with those obtained by using conventional methods.

  19. Influence of strained drain on performance of ballistic channel devices

    International Nuclear Information System (INIS)

    We have studied the performance of ballistic channel diodes with strained channel or drain, based on Monte Carlo simulation. A larger increase in drain current and mean velocity of electrons in the drain region is observed for strained drain diode compared to strained channel diode. This is due to reduction of intervalley scattering and electrons transported with smaller transverse effective mass in the strained drain. This also results in lower heat generation and parasitic resistances in strained drain. We conclude that the strained drain is an efficient way to improve electrical characteristics of devices with ballistic channel. (paper)

  20. Quantum Interference and Ballistic Transmission in Nanotube Electron Waveguides

    International Nuclear Information System (INIS)

    The electron transport properties of well-contacted individual single-walled carbon nanotubes are investigated in the ballistic regime. Phase coherent transport and electron interference manifest as conductance fluctuations as a function of Fermi energy. Resonance with standing waves in finite-length tubes and localized states due to imperfections are observed for various Fermi energies. Two units of quantum conductance 2G0=4e2/h are measured for the first time, corresponding to the maximum conductance limit for ballistic transport in two channels of a nanotube

  1. Geometrical optimization of a local ballistic magnetic sensor

    International Nuclear Information System (INIS)

    We have developed a highly sensitive local magnetic sensor by using a ballistic transport property in a two-dimensional conductor. A semiclassical simulation reveals that the sensitivity increases when the geometry of the sensor and the spatial distribution of the local field are optimized. We have also experimentally demonstrated a clear observation of a magnetization process in a permalloy dot whose size is much smaller than the size of an optimized ballistic magnetic sensor fabricated from a GaAs/AlGaAs two-dimensional electron gas

  2. Spin Injection Across a Heterojunction: A Ballistic Picture

    International Nuclear Information System (INIS)

    Spin injection across heterojunctions plays a decisive role in the new field of spintronics. Within the ballistic transport regime, we state a general expression for the spin-injection rate in a heterojunction made of two ballistic electrodes. Both the spin-orbit interaction and interface scattering effect are taken into account. Our model is consistent with the well-documented results of ferromagnetic-metal junctions. It explains the recent experimental results of a dilute-magnetic-semiconductor/semiconductor junction and predicts solutions to enhance the spin-injection rate across a ferromagnetic-semiconductor junction

  3. Unfolding Green Defense

    DEFF Research Database (Denmark)

    Larsen, Kristian Knus

    2015-01-01

    consumption in military operations, defense expenditure, energy security, and global climate change. The report then proceeds to introduce the NATO Green Defence Framework before exploring specific current uses of green technologies and green strategies for defense. The report concludes that a number...... of political, military, organizational, and technological challenges and possibilities are related to the development of green solutions for defense. Based on this conclusion the report argues that it is essential to comprehensively describe how a green solution is linked to a security challenge to develop...

  4. Defense Mechanisms in Adolescence.

    Science.gov (United States)

    Cramer, Phebe

    1979-01-01

    Results showed that by ninth or tenth grade, males begin to externalize conflict while females tend to deal with conflict internally. This differentiation of defense choice by sex is clearly established by the last two years of high school. (JMB)

  5. Demonstration of the Military Ecological Risk Assessment Framework (MERAF): Apache Longbow - Hell Missile Test at Yuma Proving Ground

    Energy Technology Data Exchange (ETDEWEB)

    Efroymson, R.A.

    2002-05-09

    This ecological risk assessment for a testing program at Yuma Proving Ground, Arizona, is a demonstration of the Military Ecological Risk Assessment Framework (MERAF; Suter et al. 2001). The demonstration is intended to illustrate how risk assessment guidance concerning-generic military training and testing activities and guidance concerning a specific type of activity (e.g., low-altitude aircraft overflights) may be implemented at a military installation. MERAF was developed with funding from the Strategic Research and Development Program (SERDP) of the Department of Defense. Novel aspects of MERAF include: (1) the assessment of risks from physical stressors using an ecological risk assessment framework, (2) the consideration of contingent or indirect effects of stressors (e.g., population-level effects that are derived from habitat or hydrological changes), (3) the integration of risks associated with different component activities or stressors, (4) the emphasis on quantitative risk estimates and estimates of uncertainty, and (5) the modularity of design, permitting components of the framework to be used in various military risk assessments that include similar activities. The particular subject of this report is the assessment of ecological risks associated with a testing program at Cibola Range of Yuma Proving Ground, Arizona. The program involves an Apache Longbow helicopter firing Hellfire missiles at moving targets, i.e., M60-A1 tanks. Thus, the three component activities of the Apache-Hellfire test were: (1) helicopter overflight, (2) missile firing, and (3) tracked vehicle movement. The demonstration was limited, to two ecological endpoint entities (i.e., potentially susceptible and valued populations or communities): woody desert wash communities and mule deer populations. The core assessment area is composed of about 126 km{sup 2} between the Chocolate and Middle Mountains. The core time of the program is a three-week period, including fourteen days of

  6. Surfing China's National Defense

    Institute of Scientific and Technical Information of China (English)

    Ji Guilin

    2010-01-01

    @@ Following the start of its first test run on August 20, 2009, the website www.mod.gov.cn of the Ministry of National Defense (MOD) of the People's Republic of China has logged more than 2 billion hits,from many countries and regions including China, the United States,the United Kingdom, Japan, Australia and Singapore. China National Defense News reporters recently interviewed Ji Guilin, the website's Editor in Chief, on its performance and the feedback of netizens.

  7. Auxins in defense strategies

    OpenAIRE

    Čarná, M. (Mária); Repka, V.; Skůpa, P. (Petr); Šturdík, E.

    2014-01-01

    Plant hormones operate in a very complex network where they regulate and control different vital mechanisms. They coordinate growth, development and defense via signaling involving different interactions of molecules. Activation of molecules responsible for regulation of plant immunity is mainly provided by salicylic and jasmonic acid signaling pathways. Similar to the signaling of these defense-associated plant hormones, auxin can also affect resistance to different pathogen groups and disea...

  8. Full-scale impact test data for tornado-missile design of nuclear plants

    International Nuclear Information System (INIS)

    It is standard practice to consider the effects of low-probability impacts of tornado-borne debris (''tornado missiles'' such as utility poles and steel pipes) in the structural design of nuclear power plants in the United States. To provide data that can be used directly in the design procedure, a series of full-scale tornado-missile impact tests was performed. This paper is a brief summary of the results and conclusions from these tests. The tests consisted of reinforced concrete panels impacted by poles, pipes, and rods propelled by a rocket sled. The panels were constructed to current minimum standards and had thicknesses typical of auxiliary buildings of nuclear power plants. A specific objective was the determination of the impact velocities below which the panels do not experience backface scabbing. Another objective was to assess the adequacy of (1) conventional design formulae for penetration and scabbing and (2) conventional design methods for overall structural response. Test missiles and velocities represented those in current design standards. Missiles included utility poles, steel pipes, and steel bars. It is important to interpret the data in this paper in recognition that the test conditions represent conservative assumptions regarding maximum wind speeds, injection of the missile into the wind stream, aerodynamic trajectory, and orientation of missile at impact. Even with the severe assumptions made, the full-scale tests described demonstrate the ability of prototypical nuclear plant walls and roofs to provide adequate protection against postulated tornado-missile impact

  9. On the Trajectories of Projectiles Depicted in Early Ballistic Woodcuts

    Science.gov (United States)

    Stewart, Sean M.

    2012-01-01

    Motivated by quaint woodcut depictions often found in many late 16th and 17th century ballistic manuals of cannonballs fired in air, a comparison of their shapes with those calculated for the classic case of a projectile moving in a linear resisting medium is made. In considering the asymmetrical nature of such trajectories, the initial launch…

  10. Ballistic hole magnetic microscopy on metal-semiconductor interfaces

    NARCIS (Netherlands)

    Banerjee, T.; Ul Haq, E.; Siekman, M.H.; Lodder, J.C.; Jansen, R.

    2005-01-01

    The transport of hot holes across metal-semiconductor interfaces is studied using ballistic hole emission microscopy. From the tip of a scanning tunneling microscope nonequilibrium holes are injected into a thin metallic overlayer on a p-type Si semiconductor, inducing a current of holes into the Si

  11. The application of computed tomography in wound ballistics research

    Science.gov (United States)

    Tsiatis, Nick; Moraitis, Konstantinos; Papadodima, Stavroula; Spiliopoulou, Chara; Kelekis, Alexis; Kelesis, Christos; Efstathopoulos, Efstathios; Kordolaimi, Sofia; Ploussi, Agapi

    2015-09-01

    In wound ballistics research there is a relationship between the data that characterize a bullet and the injury resulted after shooting when it perforates the human body. The bullet path in the human body following skin perforation as well as the damaging effect cannot always be predictable as they depend on various factors such as the bullet's characteristics (velocity, distance, type of firearm and so on) and the tissue types that the bullet passes through. The purpose of this presentation is to highlight the contribution of Computed Tomography (CT) in wound ballistics research. Using CT technology and studying virtual “slices” of specific areas on scanned human bodies, allows the evaluation of density and thickness of the skin, the subcutaneous tissue, the muscles, the vital organs and the bones. Density data taken from Hounsfield units can be converted in g/ml by using the appropriate software. By evaluating the results of this study, the anatomy of the human body utilizing ballistic gel will be reproduced in order to simulate the path that a bullet follows. The biophysical analysis in wound ballistics provides another application of CT technology, which is commonly used for diagnostic and therapeutic purposes in various medical disciplines.

  12. The ballistic performance of the bombard Mons Meg

    Directory of Open Access Journals (Sweden)

    Ian Lewtas

    2016-04-01

    Full Text Available The bombard Mons Meg, located in Edinburgh Castle, with a diameter of 19 inches (48 cm, was one of the largest calibre cannons ever built. Constructed in 1449 and presented to King James II of Scotland in 1454, Mons Meg was used in both military and ceremonial roles in Scotland until its barrel burst in 1680. This paper examines the history, internal, external and terminal ballistics of the cannon and its shot. The likely muzzle velocity was estimated by varying the propellant type and the cannon profile was investigated to identify weak spots in the design that may have led to its failure. Using the muzzle velocity calculated from the internal ballistics, simulations were performed with granite and sandstone shot for varying launch angle and ground temperature. The likely trajectory and range of the cannonballs are described. The internal and external ballistics informed the initial conditions of the terminal ballistic impact scenarios. The performance of the cannonball against both period and modern targets, in the form of a pseudo-castle wall and a monolithic concrete target, respectively, were simulated and are presented and discussed.

  13. Models of Ballistic Propagation of Heat at Low Temperatures

    Science.gov (United States)

    Kovács, R.; Ván, P.

    2016-09-01

    Heat conduction at low temperatures shows several effects that cannot be described by the Fourier law. In this paper, the performance of various theories is compared in case of wave-like and ballistic propagation of heat pulses in NaF.

  14. The ballistic performance of the bombard Mons Meg

    Institute of Scientific and Technical Information of China (English)

    Ian LEWTAS; Rachael MCALISTER; Adam WALLIS; Clive WOODLEY; Ian CULLIS

    2016-01-01

    The bombard Mons Meg, located in Edinburgh Castle, with a diameter of 19 inches (48 cm), was one of the largest calibre cannons ever built. Constructed in 1449 and presented to King James II of Scotland in 1454, Mons Meg was used in both military and ceremonial roles in Scotland until its barrel burst in 1680. This paper examines the history, internal, external and terminal ballistics of the cannon and its shot. The likely muzzle velocity was estimated by varying the propellant type and the cannon profile was investigated to identify weak spots in the design that may have led to its failure. Using the muzzle velocity calculated from the internal ballistics, simulations were performed with granite and sandstone shot for varying launch angle and ground temperature. The likely trajectory and range of the cannonballs are described. The internal and external ballistics informed the initial conditions of the terminal ballistic impact scenarios. The performance of the cannonball against both period and modern targets, in the form of a pseudo-castle wall and a monolithic concrete target, respectively, were simulated and are presented and discussed.

  15. On the Internal Ballistics of a Supergun Using Multitubular Powders

    OpenAIRE

    Sharma, B.K.

    1980-01-01

    The basic equations of internal ballistics of the German Supergun using multitubular propellants have been set up. The equations have been expressed in terms of dimensionless variables and an analytical solution has also been given assuming a linear rate of burning and neglecting the co-volume correction.

  16. Ballistic propagation of turbulence front in tokamak edge plasmas

    International Nuclear Information System (INIS)

    The flux-driven nonlinear simulation of resistive ballooning mode turbulence with tokamak edge geometry is performed to study the non-steady component in the edge turbulence. The large-scale and dynamical events in transport are investigated in a situation where the mean flow is suppressed. Two types of dynamics are observed. One is the radial propagation of the pulse of pressure gradient, the other is the appearance/disappearance of radially elongated global structure of turbulent heat flux. The ballistic propagation is observed in the pulse of pressure gradient, which is associated with the front of turbulent heat flux. We focus on this ballistic propagation phenomenon. Both of the bump of pressure gradient and the front of heat flux propagate inward and outward direction. It is confirmed that the strong fluctuation propagates with the pulse front. It is observed that the number of pulses going outward is close to those going inward. This ballistic phenomenon does not contradict to the turbulence spreading theory. Statistical characteristics of the ballistic propagation of pulses are evaluated and compared with scaling laws which is given by the turbulence spreading theory. It is found that they give qualitatively good agreement. (paper)

  17. On the Internal Ballistics of a Supergun Using Multitubular Powders

    Directory of Open Access Journals (Sweden)

    B. K. Sharma

    1980-10-01

    Full Text Available The basic equations of internal ballistics of the German Supergun using multitubular propellants have been set up. The equations have been expressed in terms of dimensionless variables and an analytical solution has also been given assuming a linear rate of burning and neglecting the co-volume correction.

  18. Learning without knowing: subliminal visual feedback facilitates ballistic motor learning

    DEFF Research Database (Denmark)

    Lundbye-Jensen, Jesper; Leukel, Christian; Nielsen, Jens Bo

    During daily life we are constantly bombarded by sensory input providing information on the state of our body and the surrounding world. Although we do not consciously perceive all sensory inputs, these may nevertheless have consequences for our future behavior (e.g. Goodale and Milner). It is a ...... by the learner, indeed facilitated ballistic motor learning. This effect likely relates to multiple (conscious versus unconscious) processing of visual feedback and to the specific neural circuitries involved in optimization of ballistic motor performance....... by subconscious (subliminal) augmented visual feedback on motor performance. To test this, 45 subjects participated in the experiment, which involved learning of a ballistic task. The task was to execute simple ankle plantar flexion movements as quickly as possible within 200 ms and to continuously improve...... ballistic rate of force development (RFD) throughout a series of 40 trials. Following each trial subjects were provided visual augmented feedback on their performance in the form of dots presented on a monitor. The y-axis amplitude of the dots represented the obtained RFD. Participants were individually...

  19. Adaptive nonlinear control of missiles using neural networks

    Science.gov (United States)

    McFarland, Michael Bryan

    Research has shown that neural networks can be used to improve upon approximate dynamic inversion for control of uncertain nonlinear systems. In one architecture, the neural network adaptively cancels inversion errors through on-line learning. Such learning is accomplished by a simple weight update rule derived from Lyapunov theory, thus assuring stability of the closed-loop system. In this research, previous results using linear-in-parameters neural networks were reformulated in the context of a more general class of composite nonlinear systems, and the control scheme was shown to possess important similarities and major differences with established methods of adaptive control. The neural-adaptive nonlinear control methodology in question has been used to design an autopilot for an anti-air missile with enhanced agile maneuvering capability, and simulation results indicate that this approach is a feasible one. There are, however, certain difficulties associated with choosing the proper network architecture which make it difficult to achieve the rapid learning required in this application. Accordingly, this technique has been further extended to incorporate the important class of feedforward neural networks with a single hidden layer. These neural networks feature well-known approximation capabilities and provide an effective, although nonlinear, parameterization of the adaptive control problem. Numerical results from a six-degree-of-freedom nonlinear agile anti-air missile simulation demonstrate the effectiveness of the autopilot design based on multilayer networks. Previous work in this area has implicitly assumed precise knowledge of the plant order, and made no allowances for unmodeled dynamics. This thesis describes an approach to the problem of controlling a class of nonlinear systems in the face of both unknown nonlinearities and unmodeled dynamics. The proposed methodology is similar to robust adaptive control techniques derived for control of linear

  20. Senate Voting On the Strategic Defense Initiative: The Impact of the 1991 Gulf War

    Directory of Open Access Journals (Sweden)

    James F. Pasley

    2012-04-01

    Full Text Available This paper examines the effects of the success of the Patriot missile system in the 1991 Gulf War on Senate roll call votes for the Strategic Defense Initiative (SDI. Previous studies have shown that both Party Identification (PID and Ideology have had a significant effect on senators' votes on defense weapons systems. Using Logit regression techniques, this paper examines whether PID and Ideology, both of which are central to political identity, remained significant factors in three Senate votes on SDI; this paper is unique compare to previous studies of such matters in that it adds two additional explanatory variables to existing models: (1 the extent to which each state might benefit from SDI and (2 whether or not the senator from each state was up for re-election in 1992 It is hypothesized that the findings will suggest that external factors played a role in the SDI Senate votes in question. Specifically, it is hypothesized that the effects of the Gulf War Patriot missile successes led to greater legislative support (compared to support levels from previous years for the Strategic Defense Initiative among Democrats, those senators whose states would benefit from SDI funding, and those senators seeking re-election.

  1. A ram-air-spoiler roll stabilization device for forward control cruciform missiles

    Science.gov (United States)

    Blair, A. B., Jr.; Sawyer, W. C.; Jackson, C. M., Jr.

    1978-01-01

    An experimental investigation has been made at supersonic Mach numbers to determine the feasibility of using a ram-air-spoiler roll control device on a typical canard control missile configuration. As a basis for roll control comparisons, conventional aileron controls on the tail fins were also tested. Results are presented which indicate that the addition of nacelles on the missile tail fins resulted in satisfactory roll control effectiveness and only small changes in basic missile stability. The ram-air-spoiler roll control effectiveness is relatively constant over the range of vehicle attitudes and Mach numbers investigated.

  2. Study on Missile Intelligent Fault Diagnosis System Based on Fuzzy NN Expert System

    Institute of Scientific and Technical Information of China (English)

    2001-01-01

    In order to study intelligent fault diagnosis methods based on fuzzy neural network (NN) expert systemand build up intelligent fault diagnosis for a type of mis-sile weapon system, the concrete implementation of a fuzzyNN fault diagnosis expert system is given in this paper. Based on thorough research of knowledge presentation, theintelligent fault diagnosis system is implemented with artificial intelligence for a large-scale missile weapon equipment.The method is an effective way to perform fuzzy fault diagnosis. Moreover, it provides a new way of the fault diagnosisfor large-scale missile weapon equipment.

  3. Design of a missile's holographic detecting/tracking and control system

    Science.gov (United States)

    Qian, Xianyi; Jiang, Xiaoyan; Bao, Yujun

    2008-12-01

    Missile must lock onto its target rapidly by holographic tracking, process its tracking signal simultaneously, be controlled with high speed. This can make missile have high mobility, high accuracy and high hit rate. Holographic detector which be designed on the detection principles of infrared signal, radar signal and laser pulse signal can detect these kinds of signals, and the holographic information detected by holographic detector be coded and output can control missile's flight. Hardware circuits compose the whole design, this can not only prevent undesired signals, but also increase rate of reaction.

  4. Summary of Flutter Experiences as a Guide to the Preliminary Design of Lifting Surfaces on Missiles

    Science.gov (United States)

    Martin, Dennis J

    1958-01-01

    Presented is a limited review of some experiences in flight testing of missiles and of wing flutter investigations that may be of interest in missile design. Several types of flutter of concern in missile studies are briefly described. Crude criteria are presented for two of the most common types of flutter to permit a rapid estimate to be made of the probability of the occurrence of flutter. Many of the details of the flutter problem have been omitted, and only the broader elements have been retained so as to give the designer an overall view of the subject.

  5. Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail

    Institute of Scientific and Technical Information of China (English)

    2006-01-01

    To study the rolling control characteristics of a canard-controlled missile, a series of wind tunnel experiment is conducted. The experimental method, the structure features of wind tunnel model and the experimental results are introduced in this paper. The experimental data show that the canard is an inefficient rolling control device for canard-controlled missile with fixed tail fins; but for the free-spinning tail fin configuration, the canard can conduct rolling control of the missile, and even have higher controlling efficiency under larger canard deflection angle.

  6. Signs of muscle thixotropy during human ballistic wrist joint movements.

    Science.gov (United States)

    Axelson, H W

    2005-11-01

    A study was conducted on healthy subjects to determine whether voluntary ballistic wrist flexion movements are influenced by immediately preceding conditioning of the forearm muscles. Single rapid wrist flexion movements were made in response to an auditory "Go" signal. Rectified surface EMG was recorded from wrist flexors and extensors, and joint position was measured by a goniometer. The movements were preceded (2-3 s) by four different conditioning routines: 40-s rest (Rest), 10-s voluntary alternating wrist joint flexion and extension movements (Osc), and 10 s of 25 degrees weak isometric wrist extensor (Ext) or flexor contractions (Flex). When subjects made ballistic movements after Osc compared with Rest, peak velocity was higher (P = 0.02) and movement time shorter (P = 0.06), but there was no difference (P = 0.83) in motor reaction time (time between the onset of the first agonist burst and movement onset). If the movements were preceded by Ext compared with Flex, motor reaction time was longer (P = 0.01), indicating a longer electromechanical delay. There were no indications that postconditioning differences in agonist or antagonist muscle activity could explain the results. It was also demonstrated that, after Rest, peak velocity was lower (P < 0.01) for the first than for the second of a series of repetitive ballistic movements. The observations corresponded to results from passive experiments in which the median nerve was electrically stimulated. In conclusion, history-dependent (thixotropic) changes in skeletal muscle resistance seem to have implications for voluntary ballistic wrist movements. The study also provided evidence that muscle conditioning influences the central nervous reaction time preceding ballistic contractions.

  7. The role of computed tomography in terminal ballistic analysis.

    Science.gov (United States)

    Rutty, G N; Boyce, P; Robinson, C E; Jeffery, A J; Morgan, B

    2008-01-01

    Terminal ballistics concerns the science of projectile behaviour within a target and includes wound ballistics that considers what happens when a projectile strikes a living being. A number of soft tissue ballistic simulants have been used to assess the damage to tissue caused by projectiles. Standard assessment of these materials, such as ballistic soap or ordnance gelatine, requires the block to be opened or that a mould to be made to visualize the wound track. This is time consuming and may affect the accuracy of the findings especially if the block dries and alters shape during the process. Therefore, accurate numerical analysis of the permanent or temporary cavity is limited. Computed tomography (CT) potentially offers a quicker non-invasive analysis tool for this task. Four commercially purchased ballistic glycerine soap blocks were used. Each had a single firearm discharged into it from a distance of approximately 15 cm using both gunshot and shotgun projectiles. After discharge, each block was imaged by a modern 16 slice multi-detector CT scanner and analysed using 3-D reconstruction software. Using the anterior-posterior and lateral scout views and the multi-plane reconstructed images, it was possible to visualize the temporary cavity, as well as the fragmentation and dispersal pattern of the projectiles, the distance travelled and angle of dispersal within the block of each projectile or fragment. A virtual cast of the temporary cavity can be also be made. Multi-detector CT with 3-D analysis software is shown to create a reliable permanent record of the projectile path allowing rapid analysis of different firearms and projectiles. PMID:17205351

  8. A Game-Theoretic History of the Cuban Missile Crisis

    Directory of Open Access Journals (Sweden)

    Frank C. Zagare

    2014-01-01

    Full Text Available This study surveys and evaluates previous attempts to use game theory to explain the strategic dynamic of the Cuban missile crisis, including, but not limited to, explanations developed in the style of Thomas Schelling, Nigel Howard and Steven Brams. All of the explanations were judged to be either incomplete or deficient in some way. Schelling’s explanation is both empirically and theoretically inconsistent with the consensus interpretation of the crisis; Howard’s with the contemporary understanding of rational strategic behavior; and Brams’ with the full sweep of the events that define the crisis. The broad outlines of a more general explanation that addresses all of the foundational questions associated with the crisis within the confines of a single, integrated, game-theoretic model with incomplete information are laid out.

  9. Parametric control systems design with applications in missile control

    Institute of Scientific and Technical Information of China (English)

    DUAN GuangRen; YU HaiHua; TAN Feng

    2009-01-01

    This paper considers parametric control of high-order descriptor linear systems via proportional plus derivative feedback.By employing general parametric solutions to a type of so-called high-order Sylvester matrix equations,complete parametric control approaches for high-order linear systems are presented.The proposed approaches give simple complete parametric expressions for the feedback gains and the closed-loop eigenvector matrices,and produce all the design degrees of freedom.Furthermore,Important special cases are particularly treated.Based on the proposed parametric design approaches,a parametric method for the gain-scheduling controller design of a linear time-varying system is proposed and the design of a BTT missile autopilot is carried out.The simulation results show that the method is superior to the traditional one in sense of either global stability or system performance.

  10. An integrated design for missile guidance/control/tracking system

    Science.gov (United States)

    Xu, Yefeng; Qiu, Haitao

    2008-10-01

    An integrated information system (IIS) which contains strapdown inertial navigation system (SINS), automatic pilot and terminal guidance seeker is proposed. Using rotating modulation approach, the performance of the low cost MEMS inertial sensor is improved by 20-30 times. The precision of the modulated MEMS gyro is available for strapdown navigation system and autopilot. The IIS gyros replace gimbal-based gyros are used in the line-of-sight (LOS) stabilization system. The seeker's LOS angular rate is estimated by combining the missile-fixed gyro information with gimbal coordinate rate information. The indirect LOS stabilization control loop is elaborately designed according to the gimbal kinematical relationship and dynamics models. The study and analysis results show that the compensation torque is available to null the disturbance and make the LOS stabilization. The proposed IIS saves two sets of gyros and make the SINS, autopilot, seeker integrated designing. It owns many advantages such as compact configuration, prominent low cost etc.

  11. Ogive Nose Hard Missile Penetrating Concrete Slab Numerical Simulation Approach

    Directory of Open Access Journals (Sweden)

    Qadir Bux

    2011-01-01

    Full Text Available Great demand exists for more efficient design to protect delicate and serious structures such as nuclear plants, Power plants, Weapon Industries, weapons storage places, water retaining structures, & etc, against impact of kinetic missiles generated both accidentally and deliberately such as dynamic loading, incident occurs in nuclear plants, terrorist attack, Natural disasters like tsunami and etc., in various impact and blast scenarios for both civilian and military activities. In many cases, projectiles can be treated as rigid bodies when their damage and erosion are not severe. Due to the intricacy of the local impact damages, investigations are generally based on experimental data. Conclusions of the experimental observations are then used to guide engineering models. Local damages studies normally fall into three categories, i.e. empirical formulae based on data fitting, idealised analytical models based on physic laws and numerical simulations based on computational mechanics and material models. In the present study, 2D asymmetrical numerical simulation have done on concrete slab against the impact of  ogive nose hard missile of 26.90mm and 76.20mm diameter with CRH ratio 2.0 and 6.0 respectively, for penetration by using Concrete Damaged Plasticity Model, and ABAQUS/Explicit dynamic analysis in ABAQUS. It is found that the strains/stresses are induced in the concrete slab and a very nicely propagation of the stresses inside the  concrete slab in the form of waves, which is a clear indication for vibrations of the concrete. The lack of failure criterion in concrete damaged plasticity model does not allow the removal of elements during the analyses. This means that spalling, scabbing, and perforation cannot be modelled with the Concrete Damage Plasticity Model. The penetration depth results shows that the deeper penetration requires higher critical impact kinetic energies, and comparison shows the simulation results are more accurate

  12. A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles

    Directory of Open Access Journals (Sweden)

    Chang-sheng Gao

    2016-01-01

    Full Text Available A guidance law for attacking ground target based on motion camouflage strategy is proposed in this paper. According to the relative position between missile and target, the dual second-order dynamics model is derived. The missile guidance condition is given by analyzing the characteristic of motion camouflage strategy. Then, the terminal guidance law is derived by using the relative motion of missile and target and the guidance condition. In the process of derivation, the three-dimensional guidance law could be designed in a two-dimensional plane and the difficulty of guidance law design is reduced. A two-dimensional guidance law for three-dimensional space is derived by bringing the estimation for target maneuver. Finally, simulation for the proposed guidance law is taken and compared with pure proportional navigation. The simulation results demonstrate that the proposed guidance law can be applied to air-to-ground missiles.

  13. Reaction jet and aerodynamics compound control missile autopilot design based on adaptive fuzzy sliding mode control

    Science.gov (United States)

    Wu, Zhenhui; Dong, Chaoyang

    2006-11-01

    Because of nonlinearity and strong coupling of reaction-jet and aerodynamics compound control missile, a missile autopilot design method based on adaptive fuzzy sliding mode control (AFSMC) is proposed in this paper. The universal approximation ability of adaptive fuzzy system is used to approximate the nonlinear function in missile dynamics equation during the flight of high angle of attack. And because the sliding mode control is robustness to external disturbance strongly, the sliding mode surface of the error system is constructed to overcome the influence of approximation error and external disturbance so that the actual overload can track the maneuvering command with high precision. Simulation results show that the missile autopilot designed in this paper not only can track large overload command with higher precision than traditional method, but also is robust to model uncertainty and external disturbance strongly.

  14. Optimized design of the inside surface of supersonic missile's elliptical dome

    Science.gov (United States)

    Wei, Qun; Bai, Yang; Liu, Hui; Jia, Hongguang; Xuan, Ming

    2009-07-01

    Dome is the head of a missile which has such a strong effect on the missile's drag. When missiles attack at high speed, the drag caused by sphere dome is 50%~60% of whole missile's drag [1]. In order to reduce the dome's drag, the idea of "conformal optics" is studied in some papers. The state of the art of conformal optics is described in James P.Mils paper [2]. But most people's work focus on the outside of dome's shape design. This paper presents a way to design the dome's inside surface. This paper is composed by three main parts. The first part expands the calculation of dome's outflow and the shock wave. The second section describes how the optical optimizing function made. Finally, the last section shows the result.

  15. A Computer Code For Evaluation of Design Parameters of Concrete Piercing Earth Shock Missile Warhead

    OpenAIRE

    Roy, P. K.; K. Ramarao

    1985-01-01

    A simple and reliable computer code has been devised for evaluating various design parameters, and predicting the penetration performance of concrete piercing earth shock missile-warhead and will be useful to the designers of earth penetrating weapon system.

  16. Missile injuries to the external genitalia: a five year experience in Maiduguri, North Eastern Nigeria

    Directory of Open Access Journals (Sweden)

    Hassan Mohammed Dogo

    2016-07-01

    Conclusions: Genital missile injuries are on the increase with militarization of civilian population. Goals of treatment still remain cosmesis, preservation of erectile and voiding function. [Int J Res Med Sci 2016; 4(7.000: 2964-2966

  17. Defense waste management plan

    International Nuclear Information System (INIS)

    Defense high-level waste (HLW) and defense transuranic (TRU) waste are in interim storage at three sites, namely: at the Savannah River Plant, in South Carolina; at the Hanford Reservation, in Washington; and at the Idaho National Engineering Laboratory, in Idaho. Defense TRU waste is also in interim storage at the Oak Ridge National Laboratory, in Tennessee; at the Los Alamos National Laboratory, in New Mexico; and at the Nevada Test Site, in Nevada. (Figure E-2). This document describes a workable approach for the permanent disposal of high-level and transuranic waste from atomic energy defense activities. The plan does not address the disposal of suspect waste which has been conservatively considered to be high-level or transuranic waste but which can be shown to be low-level waste. This material will be processed and disposed of in accordance with low-level waste practices. The primary goal of this program is to utilize or dispose of high-level and transuranic waste routinely, safely, and effectively. This goal will include the disposal of the backlog of stored defense waste. A Reference Plan for each of the sites describes the sequence of steps leading to permanent disposal. No technological breakthroughs are required to implement the reference plan. Not all final decisions concerning the activities described in this document have been made. These decisions will depend on: completion of the National Environmental Policy Act process, authorization and appropriation of funds, agreements with states as appropriate, and in some cases, the results of pilot plant experiments and operational experience. The major elements of the reference plan for permanent disposal of defense high-level and transuranic waste are summarized

  18. 是导弹还是导弹核武器?%The Missiles or Missile Nuclear Weapon?

    Institute of Scientific and Technical Information of China (English)

    赵俊

    2014-01-01

    对人教版初中历史八年级下册教材中关于“1966年……我国有了可用于实战的导弹”的表述提出质疑,并进行了详尽的论证,建议将此处表述调整为“1966年……我国有了可用于实战的导弹核武器”。%The Chinese in junior middle school history teaching material of grade eight Questioning expression about“1966...Our country can be used to combat missile”,carried out a detailed argument, suggestions will be expressed here as“1966...Our country can be used for actual combat missile nuclear weapons.”

  19. Steady Fault Characteristic Analysis of a Missile Power System Based on a Differential Evolution Algorithm

    Institute of Scientific and Technical Information of China (English)

    XU Zhi-gao; GUAN Zheng-xi; MA Jing

    2005-01-01

    The differential evolution (DE) algorithm is applied to solving the models' equations of a whole missile power system, and the steady fault characteristics of the whole system are analyzed. The DE algorithm is robust, requires few control variables, is easy to use and lends itself very well to parallel computation. Calculation results indicate that the DE algorithm simulates faults of a missile power system very well.

  20. A Spread Acceleration Guidance Scheme for Command Guided Surface-To-Air Missiles

    OpenAIRE

    Ghose, D.; B. van Dam; Prasad, UR

    1989-01-01

    A new guidance law for command guided surface-to-air missiles is presented. It attempts to reduce the integral control effort while at the same time takes into account the maneuvers of the target. A Monte-Carlo simulation of a missile-target engagement in an inclined plane is carried out to check the performance of the new guidance law in comparison with existing laws in terms of integral control effort, interception time and miss distance.

  1. 76 FR 28960 - Defense Intelligence Agency National Defense Intelligence College Board of Visitors Closed Meeting

    Science.gov (United States)

    2011-05-19

    ... of the Secretary Defense Intelligence Agency National Defense Intelligence College Board of Visitors Closed Meeting AGENCY: National Defense Intelligence College, Defense Intelligence Agency, Department of... a closed meeting of the Defense Intelligence Agency National Defense Intelligence College Board...

  2. 75 FR 76423 - Defense Intelligence Agency National Defense Intelligence College Board of Visitors Closed Meeting

    Science.gov (United States)

    2010-12-08

    ... of the Secretary Defense Intelligence Agency National Defense Intelligence College Board of Visitors Closed Meeting AGENCY: National Defense Intelligence College, Defense Intelligence Agency, Department of... a closed meeting of the Defense Intelligence Agency National Defense Intelligence College Board...

  3. 76 FR 28757 - Defense Logistics Agency Revised Regulation 1000.22, Environmental Considerations in Defense...

    Science.gov (United States)

    2011-05-18

    ... of the Secretary Defense Logistics Agency Revised Regulation 1000.22, Environmental Considerations in Defense Logistics Agency Actions AGENCY: Defense Logistics Agency, Department of Defense. ACTION: Notice of Availability (NOA) of Revised Defense Logistics Agency Regulation. SUMMARY: The Defense...

  4. A ballistic gate-tunable contact junction in graphene

    Science.gov (United States)

    Wilmart, Quentin; Rosticher, Michael; Boukhicha, Mohamed; Inhofer, Andreas; Morfin, Pascal; Feve, Gwendal; Berroir, Jean-Marc; Placais, Bernard; Equipe de Physique Mésoscopique Team

    2015-03-01

    Field-effect control of carrier is very efficient in graphene and allows controlling the doping profile with a great accuracy and high spatial resolution. This is needed if one wants to implement Dirac fermion optics experiments or simply to improve the performance of graphene devices. In this work we realize graphene transistors equipped with a set of local back-gates that provide control of local electric fields in the 108 V / m range at the 10 nanometer scale. In particular we demonstrate ballistic contact junctions using transistors with independent channel and contact back-gates. We shall discuss the possibilities offered by this technology for ballistic electronic and opto-electronic applications.

  5. Ballistic thermal rectification in asymmetric three-terminal graphene nanojunctions

    Science.gov (United States)

    Ouyang, Tao; Chen, Yuanping; Xie, Yuee; Wei, X. L.; Yang, Kaike; Yang, Ping; Zhong, Jianxin

    2010-12-01

    Graphene nanojunctions (GNJs) are important components of future nanodevices and nanocircuits. Using the nonequilibrium Green’s function method, we investigate the phononic properties of three-terminal GNJs (TGNJs). The results show that the heat flux runs preferentially along the direction from narrow to wide terminals, presenting an evident ballistic thermal rectification effect in the asymmetric TGNJs. The rectification efficiency is strongly dependent on the asymmetry of the nanojunctions, which increases rapidly with the width discrepancy between the left and right terminals. Meanwhile, the corner form of the TGNJs also plays an important role in the rectification effect. The mechanism of this thermal rectification is explained by a qualitative analysis. Compared to previous thermal rectifiers based on other materials, the asymmetric nanojunctions based on graphene possess much high rectification ratio which can approach about 200%. These indicate that asymmetric TGNJs might be a promising candidate for excellent ballistic thermal (phononic) devices.

  6. The Ballistic Pressure Wave Theory of Handgun Bullet Incapacitation

    CERN Document Server

    Courtney, Michael

    2008-01-01

    This paper presents a summary of seven distinct chains of evidence, which, taken together, provide compelling support for the theory that a ballistic pressure wave radiating outward from the penetrating projectile can contribute to wounding and incapacitating effects of handgun bullets. These chains of evidence include the fluid percussion model of traumatic brain injury, observations of remote ballistic pressure wave injury in animal models, observations of rapid incapacitation highly correlated with pressure magnitude in animal models, epidemiological data from human shootings showing that the probability of incapacitation increases with peak pressure magnitude, case studies in humans showing remote pressure wave damage in the brain and spinal cord, and observations of blast waves causing remote brain injury.

  7. Diagnostics of ballistic resistance of constructional shields and experimental verification

    Science.gov (United States)

    Zatorski, Z.

    2006-08-01

    New diagnostic methodology of ballistic resistance of multi layered shields has been developed. The energy density absorbed through shield has been introduced, { }in general form as absorbed energy density VBL[R]2 according to Recht's and Ipson's method, and VBL[Z]2 according to author's method. The absorption of kinetic energy of bullet mp \\cdot V_p2 / 2 and momentum I transfered to dynamometer of ballistic pendelum has been used to assignation of absorbed energy density VBL[Z]2 . The effectiveness used method to assignation of absorbed energy density VBL2 has been calculated by effectiveness coefficientβ s of absorbed energy density VBL2 as well as by mass coefficients α_s^2.

  8. Ballistic deflection transistors and their application to THz amplification

    Science.gov (United States)

    Margala, M.; Wu, H.; Sobolewski, Roman

    2015-10-01

    We present implementation of recently proposed ballistic deflection transistors (BDTs) as THz amplifiers. BDT is a planar device based on InGaAs/InAlAs/InP heterostructure with quasi-ballistic transport obtained in the two-dimensional electron gas layer that facilitates ultra-short transit time and high performance needed for THz-range circuitry. The BDT performance is optimized through its structural modification and the use of high-k dielectrics. Our time-domain, electrical transient measurements demonstrate sub-THz switching performance of a BDT with a ∼1-μm-wide channel. Independently, circuit simulations using experimental parameters of BDTs with a channel width of 430 nm and with the BDTs themselves connected as a multi-stage travelling-wave amplifier, designed for 6-dB gain, predict a 2.7- THz bandwidth with a gain flatness of ±0.3 dB.

  9. Imaging ballistic carrier trajectories in graphene using scanning gate microscopy

    Energy Technology Data Exchange (ETDEWEB)

    Morikawa, Sei; Masubuchi, Satoru [Institute of Industrial Science, University of Tokyo, 4-6-1 Komaba, Meguro, Tokyo 153-8505 (Japan); Dou, Ziwei; Wang, Shu-Wei; Smith, Charles G.; Connolly, Malcolm R., E-mail: mrc61@cam.ac.uk [Cavendish Laboratory, Department of Physics, University of Cambridge, Cambridge CB3 0HE (United Kingdom); Watanabe, Kenji; Taniguchi, Takashi [National Institute for Materials Science, 1-1 Namiki, Tsukuba 305-0044 (Japan); Machida, Tomoki, E-mail: tmachida@iis.u-tokyo.ac.jp [Institute of Industrial Science, University of Tokyo, 4-6-1 Komaba, Meguro, Tokyo 153-8505 (Japan); Institute for Nano Quantum Information Electronics, University of Tokyo, 4-6-1 Komaba, Meguro, Tokyo 153-8505 (Japan)

    2015-12-14

    We use scanning gate microscopy to map out the trajectories of ballistic carriers in high-mobility graphene encapsulated by hexagonal boron nitride and subject to a weak magnetic field. We employ a magnetic focusing geometry to image carriers that emerge ballistically from an injector, follow a cyclotron path due to the Lorentz force from an applied magnetic field, and land on an adjacent collector probe. The local electric field generated by the scanning tip in the vicinity of the carriers deflects their trajectories, modifying the proportion of carriers focused into the collector. By measuring the voltage at the collector while scanning the tip, we are able to obtain images with arcs that are consistent with the expected cyclotron motion. We also demonstrate that the tip can be used to redirect misaligned carriers back to the collector.

  10. A ballistic two-dimensional-electron-gas Andreev interferometer

    International Nuclear Information System (INIS)

    We report the realization and investigation of a ballistic Andreev interferometer based on an InAs two dimensional electron gas coupled to a superconducting Nb loop. We observe strong magnetic modulations in the voltage drop across the device due to quasiparticle interference within the weak-link. The interferometer exhibits flux noise down to ∼80 μΦ0/√(Hz) and a robust behavior in temperature with voltage oscillations surviving up to ∼7 K. Besides this remarkable performance, the device represents a crucial first step for the realization of a fully-tunable ballistic superconducting magnetometer and embodies a potential advanced platform for the investigation of Majorana bound states, non-local entanglement of Cooper pairs, as well as the manipulation and control of spin triplet correlations.

  11. Ballistic transport of graphene pnp junctions with embedded local gates

    International Nuclear Information System (INIS)

    We fabricated graphene pnp devices, by embedding pre-defined local gates in an oxidized surface layer of a silicon substrate. With neither deposition of dielectric material on the graphene nor electron-beam irradiation, we obtained high-quality graphene pnp devices without degradation of the carrier mobility even in the local-gate region. The corresponding increased mean free path leads to the observation of ballistic and phase-coherent transport across a local gate 130 nm wide, which is about an order of magnitude wider than reported previously. Furthermore, in our scheme, we demonstrated independent control of the carrier density in the local-gate region, with a conductance map very much distinct from those of top-gated devices. This was caused by the electric field arising from the global back gate being strongly screened by the embedded local gate. Our scheme allows the realization of ideal multipolar graphene junctions with ballistic carrier transport.

  12. Conductance of ballistic quantum wires at non-zero temperature

    International Nuclear Information System (INIS)

    Temperature dependent conductance of ballistic quantum wire has been calculated for kT j - μ, the filling of quantum subbands (G) being taken into account; here μ(T) is the chemical potential, and Ej corresponds to the top of the quantum subband. The contribution of the filled in subbands to the ballistic conductance is described by the Landauer-Buettiker formula G = 2 e2/h, whereas the conductance decreases when the subband is partly filled in, which results in disappearance of the quantum steps in case kT coincides with the quantum subband gap. This temperature quenching of the quantum steps under the gate voltage is demonstrated when studying quantum wires in a Si (100) wafer

  13. HVI Ballistic Limit Charaterization of Fused Silica Thermal Pane

    Science.gov (United States)

    Bohl, William E.; Miller, Joshua E.; Christiansen, Eric L.; Deighton, Kevin.; Davis, Bruce

    2015-01-01

    The Orion spacecraft's windows are exposed to the micrometeroid and orbital debris (MMOD) space environments while in space as well as the Earth entry environment at the mission's conclusion. The need for a low-mass spacecraft window design drives the need to reduce conservatism when assessing the design for loss of crew due to MMOD impact and subsequent Earth entry. Therefore, work is underway at NASA and Lockheed Martin to improve characterization of the complete penetration ballistic limit of an outer fused silica thermal pane. Hypervelocity impact tests of the window configuration at up to 10 km/s and hydrocode modeling have been performed with a variety of projectile materials to enable refinement of the fused silica ballistic limit equation.

  14. Defense styles of pedophilic offenders.

    Science.gov (United States)

    Drapeau, Martin; Beretta, Véronique; de Roten, Yves; Koerner, Annett; Despland, Jean-Nicolas

    2008-04-01

    This pilot study investigated the defense styles of pedophile sexual offenders. Interviews with 20 pedophiles and 20 controls were scored using the Defense Mechanisms Rating Scales. Results showed that pedophiles had a significantly lower overall defensive functioning score than the controls. Pedophiles used significantly fewer obsessional-level defenses but more major image-distorting and action-level defenses. Results also suggested differences in the prevalence of individual defenses where pedophiles used more dissociation, displacement, denial, autistic fantasy, splitting of object, projective identification, acting out, and passive aggressive behavior but less intellectualization and rationalization. PMID:17875603

  15. Defense styles of pedophilic offenders.

    Science.gov (United States)

    Drapeau, Martin; Beretta, Véronique; de Roten, Yves; Koerner, Annett; Despland, Jean-Nicolas

    2008-04-01

    This pilot study investigated the defense styles of pedophile sexual offenders. Interviews with 20 pedophiles and 20 controls were scored using the Defense Mechanisms Rating Scales. Results showed that pedophiles had a significantly lower overall defensive functioning score than the controls. Pedophiles used significantly fewer obsessional-level defenses but more major image-distorting and action-level defenses. Results also suggested differences in the prevalence of individual defenses where pedophiles used more dissociation, displacement, denial, autistic fantasy, splitting of object, projective identification, acting out, and passive aggressive behavior but less intellectualization and rationalization.

  16. Pivotal role of ballistic and quasi-ballistic electrons on LED efficiency

    Science.gov (United States)

    Ni, X.; Li, X.; Lee, J.; Liu, S.; Avrutin, V.; Matulionis, A.; Özgür, Ü.; Morkoç, H.

    2010-08-01

    Significant progress in the power conversion efficiency and brightness of InGaN-based light emitting diodes (LEDs) has paved the way for these devices to be considered for LED lighting. In this realm, however, the efficiency must be retained at high injection levels in order to generate the lumens required. Unfortunately, LEDs undergo a monotonic efficiency degradation starting at current densities even lower than 50 A/cm 2 which would hinder LED insertion into the general lighting market. The physical origins for the loss of efficiency retention are at present a topic of intense debate given its enormous implications. This paper reviews the current status of the field regarding the mechanisms that have been put forward as being responsible for the loss of efficiency, such as Auger recombination, electron overflow (spillover), current crowding, asymmetric injection of electrons and holes, and poor transport of holes through the active region, the last one being applicable to multiple quantum well designs. While the Auger recombination received early attention, increasing number of researchers seem to think otherwise at the moment in that it alone (if any) cannot explain the progressively worsening loss of efficiency reduction as the InN mole fraction is increased. Increasing number of reports seems to suggest that the electron overflow is one of the major causes of efficiency degradation. The physical driving force for this is likely to be the relatively poor hole concentration and transport, and skewed injection favoring electrons owing to their relatively high concentration. Most intriguingly there is recent experimental convincing evidence to suggest that quasi-ballistic electrons in the active region, which are not able to thermalize within the residence time and possibly longitudinal optical phonon lifetime, contribute to the carrier overflow which would require an entirely new thought process in the realm of LEDs.

  17. A Treatise on Quantum Ballistic Motion and its Applications

    OpenAIRE

    Bracher, Christian

    2007-01-01

    The motion of a charged quantum particle in a homogeneous electric field is one of the rare examples of an analytically solvable problem in quantum mechanics in realistic three-dimensional configuration space. In the thesis, an exact expression for the propagator (energy Green function) describing this quantum ballistic motion for particles of some fixed energy emitted by a pointlike isotropic source is derived. Also, it is shown how to extend this theory to higher partial waves, thereby esta...

  18. Computerized Ballistic modeling of the Comanche tailfan shroud

    OpenAIRE

    Stephan, Allen H.

    2000-01-01

    The U.S. Army has contracted Boeing-Sikorsky to develop the RAH-66 Comanche, a new, armed reconnaissance helicopter that features stealth technology designed to improve survivability when operating in hostile environments. Ballistic testing is required on the Comanche prior to fielding. Computer based simulations are being employed in order to reduce requirements for expensive live-fire testing. This thesis uses a computer program called Dytran from MacNeal-Schwendler to simulate the effects ...

  19. Ballistic transport and electrostatics in metallic carbon nanotubes

    OpenAIRE

    Svizhenko, A.; Anantram, M. P.; Govindan, T. R.

    2005-01-01

    We calculate the current and electrostatic potential drop in metallic carbon nanotube wires self-consistently, by solving the Green's function and electrostatics equations in the ballistic case. About one tenth of the applied voltage drops across the bulk of a nanowire, independent of the lengths considered here. The remaining nine tenths of the bias drops near the contacts, thereby creating a non linear potential drop. The scaling of the electric field at the center of the nanotube with leng...

  20. Parametric Studies on Star Port Propellant Grain For Ballistic Evaluation

    OpenAIRE

    Himanshu Shekhar

    2005-01-01

    Star port propellant grains have been extensively studied for their operating as well as geometrical parameters. It is observed that reduced tail-off and better neutrality cannot be achieved simultaneously in a configuration. Parametric study is conducted to know the effect of various parameters of star-shaped propellant grains for ballistic evaluation motor. For reduced tail-off, higher characteristic velocity, lower outer diameter of the star, and lower value of angular fraction is preferre...