WorldWideScience

Sample records for aeronautics

  1. Aeronautical Information System -

    Data.gov (United States)

    Department of Transportation — The Aeronautical Information System (AIS) is a leased weather automated system that provides a means of collecting and distributing aeronautical weather information...

  2. Convergent Aeronautics Solutions Project

    Data.gov (United States)

    National Aeronautics and Space Administration — The Convergent Aeronautics Solutions (CAS) Project uses short-duration activities to establish early-stage concept and technology feasibility for high-potential...

  3. NASA thesaurus aeronautics vocabulary

    Science.gov (United States)

    1991-01-01

    The controlled vocabulary used by the NASA Scientific and Technical Information effort to index documents in the area of aeronautics is presented. The terms comprise a subset of the 1988 edition of the NASA Thesaurus and its supplements issued through the end of 1990. The Aeronautics Vocabulary contains over 4700 terms presented in a hierarchical display format. In addition to aeronautics per se, the vocabulary covers supporting terminology from areas such as fluid dynamics, propulsion engineering, and test facilities and instrumentation.

  4. Dryden Aeronautical Test Range

    Data.gov (United States)

    Federal Laboratory Consortium — Recently redesignated to honor Dr. Hugh L. Dryden, NASA's Dryden Aeronautical Test Range (DATR) supports aerospace flight research and technology integration, space...

  5. Aeronautical Information System Replacement

    Data.gov (United States)

    Department of Transportation — Aeronautical Information System Replacement is a web-enabled, automation means for the collection and distribution of Service B messages, weather information, flight...

  6. National Advisory Committee for Aeronautics

    Science.gov (United States)

    1938-01-01

    NASA was created from the National Advisory Committee on Aeronautics in 1958. This is a photo of the members of the advisory board of NACA in 1938. NACA was the governmental organization charged with the supervision and conduct of scientific laboratory research in aeronautics. Its laboratories located at Langley Field, Virginia, provide new knowledge underlying the continuous improvement in the performance, efficiency, and safety of American aircraft. At this meeting Dr. Joesph S. Ames, President Emeritus of John Hopkins University, was re-elected Chairman, and Dr. Vannevar Bush, President- elect of the Carnegie Institution of Washington, was elected Vice Chairman. Dr. Ames' re-election as chairman was a recognition of his outstanding contributions to the science of aeronautics. He has been the leading scientific member of the Committee for over twenty-three years and chairman for eleven years. Under his visionary leadership the great laboratories of the N.A.C.A. at Langley Field have been developed. Left to Right: Hon. C. M. Hester, Administrator, Civil Aeronautics Authority Captain S. M. Kraus, U.S.N. Brig. General A. W. Robins, Chief, Materiel Division, Army Air Corps. Dr. L.J. Biggs, Director, National Bureau of Standards Dr. E.P. Warner Dr. Orville Wright Dr. Joesph S. Ames, Chairman Dr. C.J. Abbot, Secretary, Smithsonian Institution J.F. Victory, Secretary Rear Adm. A.B. Cook, U.S.N., Chief, Bureau Aeronautics Authority Dr. Vannevar Bush Dr. J.C. Hunsaker Dr. G.W. Lewis, Director of Aeronautical Research. Absent: Col. Charles A. Lindbergh and Maj. Gen. H. 'Hap' Arnold, Chief, Army Air Corps. One Vacany: U.S. Weather Bureau.

  7. Aeronautics. America in Space: The First Decade.

    Science.gov (United States)

    Anderton, David A.

    The major research and developments in aeronautics during the late 1950's and 1960's are reviewed descriptively with a minimum of technical content. Topics covered include aeronautical research, aeronautics in NASA, The National Advisory Committee for Aeronautics, the X-15 Research Airplane, variable-sweep wing design, the Supersonic Transport…

  8. 14 CFR 61.185 - Aeronautical knowledge.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Aeronautical knowledge. 61.185 Section 61... Flight Instructors With a Sport Pilot Rating § 61.185 Aeronautical knowledge. (a) A person who is... aeronautical knowledge areas for a recreational, private, and commercial pilot certificate applicable to...

  9. 14 CFR 61.125 - Aeronautical knowledge.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Aeronautical knowledge. 61.125 Section 61... Aeronautical knowledge. (a) General. A person who applies for a commercial pilot certificate must receive and... aeronautical knowledge areas of paragraph (b) of this section that apply to the aircraft category and...

  10. 14 CFR 61.155 - Aeronautical knowledge.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Aeronautical knowledge. 61.155 Section 61....155 Aeronautical knowledge. (a) General. The knowledge test for an airline transport pilot certificate is based on the aeronautical knowledge areas listed in paragraph (c) of this section that...

  11. NASA/University Conference on Aeronautics

    Science.gov (United States)

    1975-01-01

    The proceedings of a conference on the future of aeronautics are presented. The subjects discussed include the following: (1) aeronautics and the education of the engineer, (2) technical trends in aeronautics, and (3) the role of the university in aeronautics. The technical trends in aeronautics are concerned with aircraft noise control, the effect of the aircraft on the environment, airborne electronics for automated flight, and trends in aircraft design.

  12. Emissivity measurements on aeronautical alloys

    Energy Technology Data Exchange (ETDEWEB)

    Campo, L. del, E-mail: leire.del-campo@cnrs-orleans.f [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Perez-Saez, R.B., E-mail: raul.perez@ehu.e [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Instituto de Sintesis y Estudio de Materiales, Universidad del Pais Vasco, Apdo. 644, 48080 Bilbao (Spain); Gonzalez-Fernandez, L. [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Esquisabel, X.; Fernandez, I. [Industria de Turbo Propulsores, S.A., Planta de Zamudio, Edificio 300, 48170 Zamudio, Bizkaia (Spain); Gonzalez-Martin, P. [Industria de Turbo Propulsores, S.A., Parque empresarial San Fernando, Avda. Castilla 2, 28830 San Fernando de Henares, Madrid (Spain); Tello, M.J. [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Instituto de Sintesis y Estudio de Materiales, Universidad del Pais Vasco, Apdo. 644, 48080 Bilbao (Spain)

    2010-01-21

    The emissivity of three Ni and Co based aeronautical alloys is analyzed in this paper. These alloys are employed in high temperature environments whenever good corrosion resistance, high temperature resistance and high strength are essential. Thus, apart from the aeronautical industry, these alloys are also used in other technological applications, as for example, aerospace, nuclear reactors, and tooling. The results in this paper extend the emissivity data for these alloys available in the literature. Emissivity dependence on the radiation wavelength (2-22 {mu}m), sample temperature (200-650 {sup o}C) and emission angle (0-85{sup o}) has been investigated. In addition, the effect of surface finish and oxidation has also been taken into consideration. The data in this paper have several applications, as temperature measurement of a target by pyrometry, low observability of airplanes and thermal radiation heat transfer simulation in airplane nozzles or furnaces.

  13. Aeronautical applications of high-temperature superconductors

    Science.gov (United States)

    Turney, George E.; Luidens, Roger W.; Uherka, Kenneth; Hull, John

    1989-01-01

    The successful development of high-temperature superconductors (HTS) could have a major impact on future aeronautical propulsion and aeronautical flight vehicle systems. A preliminary examination of the potential application of HTS for aeronautics indicates that significant benefits may be realized through the development and implementation of these newly discovered materials. Applications of high-temperature superconductors (currently substantiated at 95 K) were envisioned for several classes of aeronautical systems, including subsonic and supersonic transports, hypersonic aircraft, V/STOL aircraft, rotorcraft, and solar, microwave and laser powered aircraft. Introduced and described are the particular applications and potential benefits of high-temperature superconductors as related to aeronautics and/or aeronautical systems.

  14. Aeronautical applications of high-temperature superconductors

    Science.gov (United States)

    Turney, George E.; Luidens, Roger W.; Uherka, Kenneth; Hull, John

    1989-01-01

    The successful development of high-temperature superconductors (HTS) could have a major impact on future aeronautical propulsion and aeronautical flight vehicle systems. A preliminary examination of the potential application of HTS for aeronautics indicates that significant benefits may be realized through the development and implementation of these newly discovered materials. Applications of high-temperature superconductors (currently substantiated at 95 k) were envisioned for several classes of aeronautical systems, including subsonic and supersonic transports, hypersonic aircraft, V/STOL aircraft, rotorcraft, and solar, microwave and laser powered aircraft. Introduced and described are the particular applications and potential benefits of high-temperature superconductors as related to aeronautics and/or aeronautical systems.

  15. Leading Edge Aeronautics Research for NASA Project

    Data.gov (United States)

    National Aeronautics and Space Administration — The LEARN Project explores the creation of novel concepts and processes with the potential to create new capabilities in aeronautics research through awards to the...

  16. 14 CFR 61.105 - Aeronautical knowledge.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Aeronautical knowledge. 61.105 Section 61... Aeronautical knowledge. (a) General. A person who is applying for a private pilot certificate must receive and... knowledge areas of paragraph (b) of this section that apply to the aircraft category and class rating...

  17. Piezoelectric MEMS Microphones for Ground Testing of Aeronautical Systems Project

    Data.gov (United States)

    National Aeronautics and Space Administration — Improving the acoustical environment is critical in aeronautics. Airports and aeronautical systems manufacturers are facing ever-increasing demands to reduce noise...

  18. 76 FR 58843 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2011-09-22

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  19. 78 FR 41114 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2013-07-09

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  20. 78 FR 69885 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2013-11-21

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  1. 76 FR 16643 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2011-03-24

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  2. 75 FR 41240 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2010-07-15

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  3. 75 FR 50782 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2010-08-17

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  4. 76 FR 183 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2011-01-03

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  5. 76 FR 40753 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2011-07-11

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  6. 78 FR 10640 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2013-02-14

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  7. 77 FR 38091 - NASA Advisory Council; Aeronautics Committee; Meeting.

    Science.gov (United States)

    2012-06-26

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting. AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  8. 77 FR 61432 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2012-10-09

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics... Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  9. 14 CFR 61.97 - Aeronautical knowledge.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Aeronautical knowledge. 61.97 Section 61.97... knowledge. (a) General. A person who applies for a recreational pilot certificate must receive and log... knowledge areas of paragraph (b) of this section that apply to the aircraft category and class rating...

  10. Center for Aeronautics and Space Information Sciences

    Science.gov (United States)

    Flynn, Michael J.

    1992-01-01

    This report summarizes the research done during 1991/92 under the Center for Aeronautics and Space Information Science (CASIS) program. The topics covered are computer architecture, networking, and neural nets.

  11. Civilian Aeronautical Futures - The Responsibly Imaginable

    Science.gov (United States)

    Bushnell, Dennis M.

    2006-01-01

    Since 1940 Aeronautics has had an immense impact upon Global Human lifestyles and affairs - in both the Civilian and Military arenas. During this period Long distance Train and Ship passenger transport were largely supplanted by Air Travel and Aviation assumed a dominant role in warfare. The early 1940 s to the mid 1970 s was a particularly productive period in terms of Aeronautical Technology. What is interesting is that, since the mid 1970 s, the rate of Aeronautical Technological Progress has been far slower, the basic technology in nearly all of our current Aero Systems dates from the mid 70 s or earlier. This is especially true in terms of Configuration Aerodynamics, Aeronautics appears to have "settled" on the 707, double delta and rotary wing as the approach of choice for Subsonic long haul, supersonic cruise and VTOL respectively. Obviously there have been variants and some niche digression from this/these but in the main Aeronautics, particularly civilian Aeronautics, has become a self-professed "mature", Increasingly "Commodity", Industry. The Industry is far along an existing/deployed technology curve and focused, now for decades, on incremental/evolutionary change - largely Appliers vs. developers of technology. This is, of course, in sharp contrast to the situation in the early-to-later 20th century where Aeronautics was viewed as A Major Technological Engine, much the way IT/Bio/Nano/Energetics/Quantum Technologies are viewed today. A search for Visionary Aeronautical "Futures" papers/projections indicates a decided dearth thereof over the last 20 plus years compared to the previous quarter Century. Aeronautics is part of Aerospace and Aerospace [including Aeronautics] has seen major cutbacks over the last decades. Some numbers for the U.S. Aerospace Industry serve as examples. Order of 600,000 jobs lost, with some 180,000 more on the block over the next 10 years. Approximately 25% of the Aerospace workforce is eligible to retire and the average

  12. Quality Management System for Defence Aeronautical Industry

    Directory of Open Access Journals (Sweden)

    K.T. Thomas

    2006-01-01

    Full Text Available Indian defence aeronautical industry, while becoming a global business, demands a largeeffort to monitor quality management system (QMS and to ensure quality of aeronauticalproducts. An effort is being made to look for an effective QMS for aeronautical industry in India,which will also meet the requirements of the regulatory authority.The essential features of an effective QMS are described and compared with the presentlyavailable QMS standards for defence aeronautical industry such as QCSR: 2002 (DGAQA, India,Def Stan (MOD, UK, ISO, AQAPs (NATO and Society of Automotive Engineers (SAE aerospacestandards (AS. Evolution, relevance and review of the existing standards, to meet the requirementsof the industry as well as regulatory authority, have been made to bring out the special featuresand differences. The study leads to the most acceptable standard of SAE-AS-9100 (Rev B.With suitable modifications to include regulatory requirement of assistance for governmentquality assurance in the standard, when complied with, it will fully meet the QMS requirementsof the Indian defence aeronautical supply organisations as well as the requirements of theregulatory authority. Minor reorientation of the regulatory functions and inclusion of the QMSin the defence aeronautical supply orders are also suggested.

  13. Wireless Sensor Applications in Extreme Aeronautical Environments

    Science.gov (United States)

    Wilson, William C.; Atkinson, Gary M.

    2013-01-01

    NASA aeronautical programs require rigorous ground and flight testing. Many of the testing environments can be extremely harsh. These environments include cryogenic temperatures and high temperatures (greater than 1500 C). Temperature, pressure, vibration, ionizing radiation, and chemical exposure may all be part of the harsh environment found in testing. This paper presents a survey of research opportunities for universities and industry to develop new wireless sensors that address anticipated structural health monitoring (SHM) and testing needs for aeronautical vehicles. Potential applications of passive wireless sensors for ground testing and high altitude aircraft operations are presented. Some of the challenges and issues of the technology are also presented.

  14. NASA's Role in Aeronautics: A Workshop. Volume I--Summary.

    Science.gov (United States)

    National Academy of Sciences - National Research Council, Washington, DC. Assembly of Engineering.

    The central task of the workshop summarized in this report was to examine the relationship of the National Aeronautics and Space Administration's (NASA's) aeronautical research capabilities to the state of U.S. aviation and to make recommendations about NASA's future roles in aeronautics. Topics include NASA's role in: (1) aeronautics research and…

  15. Gulf of Mexico IFR Aeronautical Chart Index - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — The IFR Enroute Aeronautical Chart series is designed to meet the needs of users who require a digital version chart. This is the visual index to the charts for the...

  16. Future Aeronautical Communication Infrastructure Technology Investigation

    Science.gov (United States)

    Gilbert, Tricia; Jin, Jenny; Bergerm Jason; Henriksen, Steven

    2008-01-01

    This National Aeronautics and Space Administration (NASA) Contractor Report summarizes and documents the work performed to investigate technologies that could support long-term aeronautical mobile communications operating concepts for air traffic management (ATM) in the timeframe of 2020 and beyond, and includes the associated findings and recommendations made by ITT Corporation and NASA Glenn Research Center to the Federal Aviation Administration (FAA). The work was completed as the final phase of a multiyear NASA contract in support of the Future Communication Study (FCS), a cooperative research and development program of the United States FAA, NASA, and EUROCONTROL. This final report focuses on an assessment of final five candidate technologies, and also provides an overview of the entire technology assessment process, including final recommendations.

  17. SMART AERONAUTICAL CHART MANAGEMENT SYSTEM DESIGN

    Directory of Open Access Journals (Sweden)

    M. E. Pakdil

    2015-10-01

    Full Text Available Civil aviation is developing rapidly, and the number of domestic and international operations is increasing exponentially every year than the previous one. Airline companies with increased air traffic and the number of passengers increase the demand of new aircrafts. An aircraft needs not only fuel but also pilot and aeronautical information (charts, digital navigation information, flight plan, and etc. to perform flight operation. One of the most important components in aeronautical information is the terminal chart. Authorized institution in every state is responsible to publish their terminal charts for certain periods. Although these charts are produced in accordance with ICAO’s Annex 4 and Annex 15, cartographic representation and page layout differs in each state’s publication. This situation makes difficult to read them by pilots. In this paper, standard instrument departure (SID charts are analysed to produce by use of cutting-edge and competitive technologies instead of classical computer-aided drawing and vector based graphic applications that are currently used by main chart producers. The goal is to design efficient and commercial chart management system that is able to produce aeronautical charts with same cartographic representation for all states.

  18. Solar energy and the aeronautics industry. Thesis

    Science.gov (United States)

    Benedek, L.

    1985-01-01

    An introduction to the physical aspects of solar energy, incidental energy and variations in solar flux is presented, along with an explanation of the physical principles of obtaining solar energy. The history of the application of solar energy to aeronautics, including the Gossamer Penguin and the Solar Challenger is given. Finally, an analysis of the possibilities of using a reaction motor with hybrid propulsion combining solar energy with traditional fuels as well as calculations of the proposed cycle and its mode of operation are given.

  19. Aeronautical progress in the United Kingdom

    Directory of Open Access Journals (Sweden)

    Dr. Cockburn

    1953-07-01

    Full Text Available The progress in aeronautics in the United Kingdom from 1903 to the present-day has been traced. The advance in design could be traced partly to the steady improvement in techniques such as strength of materials, structural methods, aerodynamics and engine design, and partly to definite technical discontinuities such as the introduction of the unbraced monoplane and later of the jet turbine. The key to this progress has been the large investment made in science and technical research and the healthy integration between industrial enterprise and government planning.

  20. NASA's Role in Aeronautics: A Workshop. Volume IV - General Aviation.

    Science.gov (United States)

    National Academy of Sciences - National Research Council, Washington, DC. Assembly of Engineering.

    The central task of a 1980 workshop on the role of the National Aeronautics and Space Administration (NASA) in aeronautics was to examine the relationship of NASA's research capabilities to the state of U.S. aviation and to make recommendations about NASA's future role in aeronautics. The findings and recommendations of the Panel on General…

  1. NASA's Role in Aeronautics: A Workshop. Volume II - Military Aviation.

    Science.gov (United States)

    National Academy of Sciences - National Research Council, Washington, DC. Assembly of Engineering.

    The central task of a 1980 workshop on the role of the National Aeronautics and Space Administration (NASA) in aeronautics was to examine the relationship of NASA's research capabilities to the state of U.S. aviation and to make recommendations about NASA's future role in aeronautics. The findings and recommendations of the Panel on Military…

  2. Transactions of Nanjing University of Aeronautics & Astronautics

    Institute of Scientific and Technical Information of China (English)

    2004-01-01

    Transactions of Nanjing University of Aeronautics & Astronautics (TNUAA, in English) is a comprehensive academic publication which deals mainly with the research achievements in aeronautics, civil aviation, astronautics and their theoretical basis. It is published by Nanjing University of Aeronautics & Astronautics, and has started its publication since Oct. 1982.

  3. 75 FR 17166 - NASA Advisory Council; Aeronautics Committee; Meeting

    Science.gov (United States)

    2010-04-05

    ... SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Meeting AGENCY: National Aeronautics and Space Administration. ACTION: Notice of meeting. SUMMARY: In accordance with the Federal Advisory Committee Act, Public Law 92-463, as amended, the National Aeronautics and Space Administration announces...

  4. IMPLEMENTATION OF AERONAUTICAL LOCAL SATELLITE AUGMENTATION SYSTEM

    Directory of Open Access Journals (Sweden)

    Stojce Ilcev

    2011-03-01

    Full Text Available Abstract. This paper introduces development and implementation of new Local Satellite AugmentationSystem as an integration component of the Regional Satellite Augmentation System (RSAS employingcurrent and new Satellite Communications, Navigation and Surveillance (CNS for improvement of the AirTraffic Control (ATC and Air Traffic Management (ATM and for enhancement safety systems includingtransport security and control of flights in all stages, airport approaching, landing, departures and allmovements over airport surface areas. The current first generation of the Global Navigation Satellite SystemGNSS-1 applications are represented by fundamental military solutions for Position, Velocity and Time ofthe satellite navigation and determination systems such as the US GPS and Russian GLONASS (Former-USSR requirements, respectively. The establishment of Aeronautical CNS is also discussed as a part ofGlobal Satellite Augmentation Systems of GPS and GLONASS systems integrated with existing and futureRSAS and LSAS in airports areas. Specific influence and factors related to the Comparison of the Currentand New Aeronautical CNS System including the Integration of RSAS and GNSS solutions are discussedand packet of facts is determined to maximize the new satellite Automatic Dependent Surveillance System(ADSS and Special Effects of the RSAS Networks. The possible future integration of RSAS and GNSS andthe common proposal of the satellite Surface Movement Guidance and Control are presented in thechangeless ways as of importance for future enfacements of ATC and ATM for any hypothetical airportinfrastructure.Keywords: ADSS, ATC, ATM, CNS, GSAS, LRAS, RSAS, SMGC, Special Effects of RSAS.

  5. Aeronautical Research Engineer Milt Thompson computing data

    Science.gov (United States)

    1956-01-01

    Milton O. Thompson was hired as an engineer at the National Advisory Committee for Aeronautics' High-Speed Flight Station (later renamed the National Aeronautics and Space Administration's Dryden Flight Research Center) on March 19, 1956. In 1958 he became a research pilot, but in this photo Milt is working on data from another pilot's research flight. Thompson began flying with the U.S. Navy as a pilot trainee at the age of 19. He subsequently served during World War II, with duty in China and Japan. Following six years of active naval service, he entered the University of Washington, in Seattle, Washington. Milt graduated in 1953 with a Bachelor of Science degree in Engineering. He remained in the Naval Reserves during college, and continued flying--not only naval aircraft but crop dusters and forest-spraying aircraft. After college graduation, Milt became a flight test engineer for the Boeing Aircraft Company in Seattle, where he was employed for two years before coming to the High-Speed Flight Station.

  6. TEXTILE STRUCTURES FOR AERONAUTICS (PART II

    Directory of Open Access Journals (Sweden)

    SOLER Miquel

    2014-05-01

    Full Text Available Three-dimensional (3D textile structures with better delamination resistance and damage impact tolerance to be applied in composites for structural components is one of the main goals of the aeronautical industry. Textile Research Centre in Canet de Mar has been working since 2008 in this field. Our staff has been designing, developing and producing different textile structures using different production methods and machinery to improve three-dimensional textile structures as fiber reinforcement for composites. This paper describes different tests done in our textile labs from unidirectional structures to woven, knitted or braided 3 D textile structures. Advantages and disadvantages of each textile structure are summarized. The second part of this paper deals with our know-how in the manufacturing and assessing of three-dimensional textile structures during this last five years in the field of textile structures for composites but also in the development of structures for other applications. In the field of composites for aeronautic sector we have developed textile structures using the main methods of textile production, that is to say, weaving, warp knitting, weft knitting and braiding. Comparing the advantages and disadvantages it could be said that braided fabrics, with a structure in the three space axes are the most suitable for fittings and frames.

  7. TEXTILE STRUCTURES FOR AERONAUTICS (PART I

    Directory of Open Access Journals (Sweden)

    SOLER Miquel

    2014-05-01

    Full Text Available Three-dimensional (3D textile structures with better delamination resistance and damage impact tolerance to be applied in composites for structural components is one of the main goals of the aeronautical industry. Textile Research Centre in Canet de Mar has been working since 2008 in this field. Our staff has been designing, developing and producing different textile structures using different production methods and machinery to improve three-dimensional textile structures as fiber reinforcement for composites. This paper describes different tests done in our textile labs from unidirectional structures to woven, knitted or braided 3 D textile structures. Advantages and disadvantages of each textile structure are summarized. The first part of this paper deals with the introduction of our Textile Research Centre in the field of composites and carbon fiber as a main material to produce three – dimensional textile structures. The use of composite materials in aerospace structures has increased over the past decades. Our contribution related to this field consists of the development of three- dimensional textile structures and even the adaptation and improvement of machinery to do it possible. Carbon fiber provides advantages as volumetric fraction and minimum fault occurrence. However carbon fiber has also disadvantages as uncomfortable handling delamination and high cost of material and processing.

  8. Classification of Aeronautics System Health and Safety Documents

    Data.gov (United States)

    National Aeronautics and Space Administration — Most complex aerospace systems have many text reports on safety, maintenance, and associated issues. The Aviation Safety Reporting System (ASRS) spans several...

  9. Sectoral Innovation Watch Space and Aeronautics Sectors. Final sector report

    NARCIS (Netherlands)

    Giessen, A.M. van der

    2011-01-01

    The space and aeronautics sectors are high-technology sectors and belong to the most innovative sectors in Europe1. Analysis of CIS4 data shows that the space and aeronautics sectors continue to be very innovative. 85% of the firms is engaged in intramural R&D. Total R&D expenditures are between 21%

  10. Compressed Aeronautical Chart Processing Operator’s Manual

    Science.gov (United States)

    2007-11-02

    the processing thread A4A denotes a CAC ODI build for an (A) aeronautical chart at the (4) operational navigation chart (ONC) (1:1M) scale with...builds when both charts are at the same scale. For example, the processing thread A4A denotes a CAC ODI build for an (A) aeronautical chart at the (4

  11. A Hybrid Satellite-Terrestrial Approach to Aeronautical Communication Networks

    Science.gov (United States)

    Kerczewski, Robert J.; Chomos, Gerald J.; Griner, James H.; Mainger, Steven W.; Martzaklis, Konstantinos S.; Kachmar, Brian A.

    2000-01-01

    Rapid growth in air travel has been projected to continue for the foreseeable future. To maintain a safe and efficient national and global aviation system, significant advances in communications systems supporting aviation are required. Satellites will increasingly play a critical role in the aeronautical communications network. At the same time, current ground-based communications links, primarily very high frequency (VHF), will continue to be employed due to cost advantages and legacy issues. Hence a hybrid satellite-terrestrial network, or group of networks, will emerge. The increased complexity of future aeronautical communications networks dictates that system-level modeling be employed to obtain an optimal system fulfilling a majority of user needs. The NASA Glenn Research Center is investigating the current and potential future state of aeronautical communications, and is developing a simulation and modeling program to research future communications architectures for national and global aeronautical needs. This paper describes the primary requirements, the current infrastructure, and emerging trends of aeronautical communications, including a growing role for satellite communications. The need for a hybrid communications system architecture approach including both satellite and ground-based communications links is explained. Future aeronautical communication network topologies and key issues in simulation and modeling of future aeronautical communications systems are described.

  12. An Overview of the NASA Aeronautics Test Program Strategic Plan

    Science.gov (United States)

    Marshall, Timothy J.

    2010-01-01

    U.S. leadership in aeronautics depends on ready access to technologically advanced, efficient, and affordable aeronautics test capabilities. These systems include major wind tunnels and propulsion test facilities and flight test capabilities. The federal government owns the majority of the major aeronautics test capabilities in the United States, primarily through the National Aeronautics and Space Administration (NASA) and the Department of Defense (DoD), however an overarching strategy for management of these national assets was needed. Therefore, in Fiscal Year (FY) 2006 NASA established the Aeronautics Test Program (ATP) as a two-pronged strategic initiative to: (1) retain and invest in NASA aeronautics test capabilities considered strategically important to the agency and the nation, and (2) establish a strong, high level partnership with the DoD Test Resources Management Center (TRMC), stewards of the DoD test and evaluation infrastructure. Since then, approximately seventy percent of the ATP budget has been directed to underpin fixed and variable costs of facility operations within its portfolio and the balance towards strategic investments in its test facilities, including maintenance and capability upgrades. Also, a strong guiding coalition was established through the National Partnership for Aeronautics Testing (NPAT), with governance by the senior leadership of NASA s Aeronautics Research Mission Directorate (ARMD) and the DoD's TRMC. As part of its strategic planning, ATP has performed or participated in many studies and analyses, including assessments of major NASA and DoD aeronautics test capabilities, test facility condition evaluations and market research. The ATP strategy has also benefitted from unpublished RAND research and analysis by Ant n et al. (2009). Together, these various studies, reports and assessments serve as a foundation for a new, five year strategic plan that will guide ATP through FY 2014. Our vision for the future is a balanced

  13. Kennedy Educate to Innovate (KETI) Aeronautics PowerPoint Presentation

    Science.gov (United States)

    Davila, Dina

    2010-01-01

    This slide presentation reviews some fundamental features of aeronautics. It is designed to introduce students to aeronautics and to engage them in Science Technology Education and Mathematics (STEM). It reviews the history of airflight, the aircraft components and their interaction with the forces that make flight possible (i.e. lift, weight drag and thrust), and the interaction of the components that create aircraft movements (roll, pitch and yaw)

  14. NASA Ames and Future of Space Exploration, Science, and Aeronautics

    Science.gov (United States)

    Cohen, Jacob

    2015-01-01

    Pushing the frontiers of aeronautics and space exploration presents multiple challenges. NASA Ames Research Center is at the forefront of tackling these issues, conducting cutting edge research in the fields of air traffic management, entry systems, advanced information technology, intelligent human and robotic systems, astrobiology, aeronautics, space, earth and life sciences and small satellites. Knowledge gained from this research helps ensure the success of NASA's missions, leading us closer to a world that was only imagined as science fiction just decades ago.

  15. 76 FR 75565 - NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems (UAS) Subcommittee Meeting

    Science.gov (United States)

    2011-12-02

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems (UAS) Subcommittee Meeting AGENCY: National Aeronautics and Space Administration. ACTION: Notice of Meeting....

  16. 77 FR 32699 - NASA Advisory Council; Aeronautics Committee; UAS Subcommittee Meeting

    Science.gov (United States)

    2012-06-01

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; UAS Subcommittee Meeting AGENCY: National Aeronautics and Space Administration. ACTION: Notice of meeting. SUMMARY: In accordance with...

  17. 78 FR 25100 - NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems Subcommittee; Meeting

    Science.gov (United States)

    2013-04-29

    ... From the Federal Register Online via the Government Publishing Office NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems Subcommittee; Meeting AGENCY: National Aeronautics and Space Administration. ACTION: Notice of meeting....

  18. 78 FR 13383 - Public Availability of the National Aeronautics and Space Administration FY 2012 Service Contract...

    Science.gov (United States)

    2013-02-27

    ... SPACE ADMINISTRATION Public Availability of the National Aeronautics and Space Administration FY 2012 Service Contract Inventory (SCI) AGENCY: Office of Procurement, National Aeronautics and Space... National Aeronautics and Space Administration (NASA) is publishing this notice to advise the public of...

  19. The Concept of a Method Ensuring Aeronautical Data Quality

    Directory of Open Access Journals (Sweden)

    Dudek Ewa

    2016-07-01

    Full Text Available The paper presents the concept of a method ensuring quality of aeronautical data. European Union (among others UE 73/2010 as well as international (among others ICAO Annex 15 regulations introduce a number of requirements regarding the quality and safety of aeronautical data. Those directives set up a complementary regulations system. However with their objective and scope they determine mainly the specifications and requirements that are to be implemented and compatible. Mentioned regulations also refer to selected international standards (e.g. ISO 19157, focused on quality and safety of geographic data and information. Nevertheless within the scope of considered regulations and norms no algorithms and methods of ensuring required quality in the process of aeronautical data collection and processing were determined. Taking into account the identified needs, authors proposed the application of statistical method for process quality management – six-sigma.

  20. ROMANIAN AERONAUTICAL METEOROLOGY APPLICABLE LEGAL FRAMEWORK –BRIEFING

    Directory of Open Access Journals (Sweden)

    CATALIN POPA

    2012-05-01

    Full Text Available The purpose of this briefing is toprovide an overview of the aeronautical meteorology legal framework in Romania. In this context, the role and importance of aeronautical meteorology in international air traffic management will be underlined, with focus on the civil aviation activity in Romania. The international legal framework and modalities of implementing these rules at national level will constitute a significant part of the present study., Specific accent will be put on the national regulatory framework and structure, means of updating it, and how it responds to changing regulatory requirements.

  1. A Digital Library for the National Advisory Committee for Aeronautics

    Science.gov (United States)

    Nelson, Michael L.

    1999-01-01

    We describe the digital library (DL) for the National Advisory Committee for Aeronautics (NACA), the NACA Technical Report Server (NACATRS). The predecessor organization for the National Aeronautics and Space Administration (NASA), NACA existed from 1915 until 1958. The primary manifestation of NACA's research was the NACA report series. We describe the process of converting this collection of reports to digital format and making it available on the World Wide Web (WWW) and is a node in the NASA Technical Report Server (NTRS). We describe the current state of the project, the resulting DL technology developed from the project, and the future plans for NACATRS.

  2. Aeronautics Study Takes Off! Glider Design for Beginners

    Science.gov (United States)

    Lazaros, Edward J.; Carlson, Katie

    2008-01-01

    Study of aeronautics is an interesting and motivating subject for students and educators alike. The activity described in this article--appropriate for upper elementary or middle school students--provides an excellent introduction to airplane design and the science of aerodynamics. It also gives students good experience applying knowledge from a…

  3. A Case Study of Peer Learning in Higher Aeronautical Education

    Science.gov (United States)

    Borglund, Dan

    2007-01-01

    In order to improve student learning in an advanced course in aeronautics, lectures are replaced with more student-centred sessions based on peer learning. The course is organised in student teams, with the main task of delivering lecture requests for full class discussions. For the same reason, the written theory exam is replaced by a peer review…

  4. National Aeronautics and Space Administration (NASA) Education 1993-2009

    Science.gov (United States)

    Ivie, Christine M.

    2009-01-01

    The National Aeronautics and Space Administration was established in 1958 and began operating a formal education program in 1993. The purpose of this study was to analyze the education program from 1993-2009 by examining strategic plan documents produced by the NASA education office and interviewing NASA education officials who served during that…

  5. 14 CFR 61.159 - Aeronautical experience: Airplane category rating.

    Science.gov (United States)

    2010-01-01

    ... command aeronautical experience requirements of ICAO,” as prescribed under Article 39 of the Convention on International Civil Aviation, if the applicant does not meet the ICAO requirements contained in Annex 1... certificate without the ICAO limitation specified under paragraph (d) of this section when the...

  6. International law and regulation of aeronautical public correspondence by satellite

    NARCIS (Netherlands)

    Brisibe, Tare

    2006-01-01

    This work covers the evolution of satellite based Aeronautical Public Correspondence and the operational environment in which services are being offered. Followed by an examination of applicable rules, including the relevant institutions from which they emanate, attention is devoted to questions on

  7. FY 1978 aeronautics and space technology program summary

    Science.gov (United States)

    1977-01-01

    Highlights of the aeronautics program include research on aircraft energy efficiency, supersonic cruise aircraft, vertical takeoff and landing aircraft, short haul/short takeoff and landing aircraft, and general aviation aircraft. The space technology program includes work on space structures, propulsion systems, power systems, materials, and electronics.

  8. National Aeronautics and Space Administration Scientific and Technical Information Programs.

    Science.gov (United States)

    Pinelli, Thomas E., Ed.

    1990-01-01

    Eleven articles discuss informational and educational programs of the National Aeronautics and Space Administration (NASA). Some of the areas discussed include scientific and technical information management, the new Space and Earth Science Information Systems, transfer of technology to other industries, intellectual property issues, and the…

  9. Aeronautics: An Educator's Guide with Activities in Science, Mathematics, and Technology Education.

    Science.gov (United States)

    National Aeronautics and Space Administration, Washington, DC.

    This educator's guide, developed for students in grades 2-4, discusses the field of aeronautics. It begins with education standards and skill matrices for the classroom activities, a description of the National Aeronautics and Space Administration (NASA) aeronautics mission, and a brief history of aeronautics. Activities are written for the…

  10. 78 FR 15804 - Waiver of Aeronautical Land-Use Assurance: Rolla National Airport (VIH), Rolla, MO

    Science.gov (United States)

    2013-03-12

    ... Federal Aviation Administration Waiver of Aeronautical Land-Use Assurance: Rolla National Airport (VIH... airport property at the Rolla National Airport (VIH) from aeronautical use to non-aeronautical for revenue... Airport (VIH) is proposing the release of one parcel, of 10 acres, more or less from aeronautical to...

  11. Implementation of aeronautic image compression technology on DSP

    Science.gov (United States)

    Wang, Yujing; Gao, Xueqiang; Wang, Mei

    2007-11-01

    According to the designed characteristics and demands of aeronautic image compression system, lifting scheme wavelet and SPIHT algorithm was selected as the key part of software implementation, which was introduced with details. In order to improve execution efficiency, border processing was simplified reasonably and SPIHT (Set Partitioning in Hierarchical Trees) algorithm was also modified partly. The results showed that the selected scheme has a 0.4dB improvement in PSNR(peak-peak-ratio) compared with classical Shaprio's scheme. To improve the operating speed, the hardware system was then designed based on DSP and many optimization measures were then applied successfully. Practical test showed that the system can meet the real-time demand with good quality of reconstruct image, which has been used in an aeronautic image compression system practically.

  12. Tribology needs for future space and aeronautical systems

    Science.gov (United States)

    Fusaro, Robert L.

    1991-01-01

    Future aeronautical and space missions will push tribology technology beyond its current capability. The objective is to discuss the current state of the art of tribology as it is applied to advanced aircraft and spacecraft. Areas of discussion include materials lubrication mechanisms, factors affecting lubrication, current and future tribological problem areas, potential new lubrication techniques, and perceived technology requirements that need to be met in order to solve these tribology problems.

  13. New trends for the NDT of aeronautic welds

    Science.gov (United States)

    Ithurralde, G.; Simonet, D.; Choffy, J.-P.; Bernard, L.

    2001-04-01

    Recent advances in laser beam welding, electron beam welding and friction stir welding enable to join aeronautic and space alloys (mainly aluminum based) and think about new welded design for structural parts at a lower cost. This paper deals with both the non destructive testing approach implemented for welding process optimization, and the NDT multi-sensors tools selected because of their ability for on-line defect tracking automation.

  14. Numerical analysis of impact behaviour on aeronautical composite protections

    OpenAIRE

    Portilla Bullido, Alberto

    2011-01-01

    In this project, a complete study of impacts against protection composite materials is presented, taking into account all parameters involved in the process: from the organic fibre that is part of the composite, to the projectile impacting on the protection panels. The project was done during an internship in the department of Structural Dynamics and Aeroelasticity at Airbus Military (EADS-CASA), therefore most of the impacts studied here are typical from aeronautics industry. During the impa...

  15. 78 FR 38076 - NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems Subcommittee; Meeting

    Science.gov (United States)

    2013-06-25

    ... SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems... of the Aeronautics Committee of the NASA Advisory Council. The meeting will be held for the purpose... and Space Administration Headquarters, Washington, DC 20546, (202) 358-1578, or...

  16. 75 FR 63534 - Seventh Meeting-Special Committee 222: Inmarsat Aeronautical Mobile Satellite (Route) Services

    Science.gov (United States)

    2010-10-15

    ...: Inmarsat Aeronautical Mobile Satellite (Route) Services. The agenda will include: Agenda Opening Plenary... Satellite (Route) Services AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of RTCA Special Committee 222: Inmarsat Aeronautical Mobile Satellite (Route) Services meeting. SUMMARY: The...

  17. A Flexible System for Simulating Aeronautical Telecommunication Network

    Science.gov (United States)

    Maly, Kurt; Overstreet, C. M.; Andey, R.

    1998-01-01

    At Old Dominion University, we have built Aeronautical Telecommunication Network (ATN) Simulator with NASA being the fund provider. It provides a means to evaluate the impact of modified router scheduling algorithms on the network efficiency, to perform capacity studies on various network topologies and to monitor and study various aspects of ATN through graphical user interface (GUI). In this paper we describe briefly about the proposed ATN model and our abstraction of this model. Later we describe our simulator architecture highlighting some of the design specifications, scheduling algorithms and user interface. At the end, we have provided the results of performance studies on this simulator.

  18. FY11 Facility Assessment Study for Aeronautics Test Program

    Science.gov (United States)

    Loboda, John A.; Sydnor, George H.

    2013-01-01

    This paper presents the approach and results for the Aeronautics Test Program (ATP) FY11 Facility Assessment Project. ATP commissioned assessments in FY07 and FY11 to aid in the understanding of the current condition and reliability of its facilities and their ability to meet current and future (five year horizon) test requirements. The principle output of the assessment was a database of facility unique, prioritized investments projects with budgetary cost estimates. This database was also used to identify trends for the condition of facility systems.

  19. Information Systems for NASA's Aeronautics and Space Enterprises

    Science.gov (United States)

    Kutler, Paul

    1998-01-01

    The aerospace industry is being challenged to reduce costs and development time as well as utilize new technologies to improve product performance. Information technology (IT) is the key to providing revolutionary solutions to the challenges posed by the increasing complexity of NASA's aeronautics and space missions and the sophisticated nature of the systems that enable them. The NASA Ames vision is to develop technologies enabling the information age, expanding the frontiers of knowledge for aeronautics and space, improving America's competitive position, and inspiring future generations. Ames' missions to accomplish that vision include: 1) performing research to support the American aviation community through the unique integration of computation, experimentation, simulation and flight testing, 2) studying the health of our planet, understanding living systems in space and the origins of the universe, developing technologies for space flight, and 3) to research, develop and deliver information technologies and applications. Information technology may be defined as the use of advance computing systems to generate data, analyze data, transform data into knowledge and to use as an aid in the decision-making process. The knowledge from transformed data can be displayed in visual, virtual and multimedia environments. The decision-making process can be fully autonomous or aided by a cognitive processes, i.e., computational aids designed to leverage human capacities. IT Systems can learn as they go, developing the capability to make decisions or aid the decision making process on the basis of experiences gained using limited data inputs. In the future, information systems will be used to aid space mission synthesis, virtual aerospace system design, aid damaged aircraft during landing, perform robotic surgery, and monitor the health and status of spacecraft and planetary probes. NASA Ames through the Center of Excellence for Information Technology Office is leading the

  20. Reliability program requirements for aeronautical and space system contractors

    Science.gov (United States)

    1987-01-01

    General reliability program requirements for NASA contracts involving the design, development, fabrication, test, and/or use of aeronautical and space systems including critical ground support equipment are prescribed. The reliability program requirements require (1) thorough planning and effective management of the reliability effort; (2) definition of the major reliability tasks and their place as an integral part of the design and development process; (3) planning and evaluating the reliability of the system and its elements (including effects of software interfaces) through a program of analysis, review, and test; and (4) timely status indication by formal documentation and other reporting to facilitate control of the reliability program.

  1. Aeronautical Magnetic Torque Limiter for Passive Protection against Overloads

    Directory of Open Access Journals (Sweden)

    Cristian Cristache

    2016-09-01

    Full Text Available Actual aerospace and defense technologies present multiple limitations that need to be overcome in order to evolve to less contaminating and more efficient aircraft solutions. Contactless technologies come with essential advantages such as the absence of wear and friction. This work describes the design, prototype, and performance test according to RTCA-DO-160 of an aeronautical magnetic torque limiter. The results show correct continuous transmission operation (2250 rpm and 24 Nm from −50 °C to +90 °C. Moreover, overload protection has been demonstrated for more than 200 jamming events without damage or required maintenance to the device.

  2. 3 CFR - Designation of Officers of the National Aeronautics And Space Administration To Act as Administrator

    Science.gov (United States)

    2010-01-01

    ... 3 The President 1 2010-01-01 2010-01-01 false Designation of Officers of the National Aeronautics... Memorandum of January 16, 2009 Designation of Officers of the National Aeronautics And Space Administration To Act as Administrator Memorandum for the Administrator of the National Aeronautics and...

  3. 77 FR 7183 - Public Availability of the National Aeronautics and Space Administration FY 2011 Service Contract...

    Science.gov (United States)

    2012-02-10

    ... SPACE ADMINISTRATION Public Availability of the National Aeronautics and Space Administration FY 2011 Service Contract Inventory AGENCY: National Aeronautics and Space Administration. ACTION: Notice of Public... 2010 (Pub. L. 111-117), National Aeronautics and Space Administration (NASA) is publishing this...

  4. 76 FR 6827 - Public Availability of the National Aeronautic and Space Administration FY 2010 Service Contract...

    Science.gov (United States)

    2011-02-08

    ... SPACE ADMINISTRATION Public Availability of the National Aeronautic and Space Administration FY 2010 Service Contract Inventory AGENCY: National Aeronautic and Space Administration. ACTION: Notice of public... of the Consolidated Appropriations Act of 2010 (Pub. L. 111-117), National Aeronautic and...

  5. Interference Analysis for an Aeronautical Mobile Airport Communications System

    Science.gov (United States)

    Wilson, Jeffrey D.; Kercewski, Robert J.

    2010-01-01

    The next generation of aeronautical communications for airport surface applications has been identified through a NASA research program and an international collaborative future communications study. The result, endorsed by both the United States and European regulatory agencies is called AeroMACS (Aeronautical Mobile Airport Communications System) and is based upon the IEEE 802.16e mobile wireless standard. Coordinated efforts to develop appropriate aviation standards for the AeroMACS system are now underway within RTCA (United States) and Eurocae (Europe). AeroMACS will be implemented in a recently allocated frequency band, 5091- 5150 MHz. As this band is also occupied by fixed satellite service uplinks, AeroMACS must be designed to avoid interference with this incumbent service. The aspects of AeroMACS operation that present potential interference to the fixed satellite service are under analysis in order to enable the definition of standards that assure that such interference will be avoided. The NASA Glenn Research Center has been involved in this analysis, and the first results of modeling and simulation efforts directed at this analysis are the subject of this paper.12

  6. Aeronautical satellite antenna steering using magnetic field sensors

    Science.gov (United States)

    Sydor, John; Dufour, Martial

    1993-01-01

    Designers of aeronautical satellite terminals are often faced with the problem of steering a directive antenna from an airplane or helicopter. This problem is usually solved by using aircraft orientation information derived from inertial sensors on-board the aircraft in combination with satellite ephemeris information calculated from geographic coordinates. This procedure works well but relies heavily on avionics that are external to the terminal. For the majority of small aircraft and helicopters which will form the bulk of future aeronautical satcom users, such avionics either do not exist or are difficult for the satellite terminal to interface with. At the Communications Research Center (CRC), work has been undertaken to develop techniques that use the geomagnetic field and satellite antenna pointing vectors (both of which are stationary in a local geographical area) to track the position of a satellite relative to a moving platform such as an aircraft. The performance of this technique is examined and a mathematical steering transformation is developed within this paper. Details are given regarding the experimental program that will be undertaken to test the concepts proposed herein.

  7. Additional Technologies and Investigations for Provision of Future Aeronautical Communications

    Science.gov (United States)

    Gilbert, Tricia; Jin, Jenny; Berger, Jason; Henriksen, Steve

    2008-01-01

    The following NASA Contractor Report documents the in-depth studies on select technologies that could support long-term aeronautical mobile communications operating concepts. This work was performed during the third and final phase of NASA s Technology Assessment for the Federal Aviation Administration (FAA)/EUROCONTROL Future Communications Study (FCS) under a multiyear NASA contract. It includes the associated findings of ITT Corporation and NASA Glenn Research Center to the FAA as of the end of May 2007. The activities documented in this report focus on three final technology candidates identified by the United States, and were completed before sufficient information about two additional technology candidates proposed by EUROCONTROL was made available. A separate report to be published by NASA/CR-2008-215144, entitled Final Report on Technology Investigations for Provision of Future Aeronautical Communications will include an assessment of all five final candidate technologies considered by the U.S. agencies (FAA and NASA) and EUROCONTROL. It will also provide an overview of the entire technology assessment process, including final recommendations. All three phases of this work were performed in compliance with the Terms of Reference for the Action Plan number 17 (AP-17) cooperative research agreement among EUROCONTROL, FAA, and NASA along with the general guidance of the FAA and EUROCONTROL available throughout this study.

  8. Aeronautical Mobile Airport Communications System (AeroMACS)

    Science.gov (United States)

    Budinger, James M.; Hall, Edward

    2011-01-01

    To help increase the capacity and efficiency of the nation s airports, a secure wideband wireless communications system is proposed for use on the airport surface. This paper provides an overview of the research and development process for the Aeronautical Mobile Airport Communications System (AeroMACS). AeroMACS is based on a specific commercial profile of the Institute of Electrical and Electronics Engineers (IEEE) 802.16 standard known as Wireless Worldwide Interoperability for Microwave Access or WiMAX (WiMax Forum). The paper includes background on the need for global interoperability in air/ground data communications, describes potential AeroMACS applications, addresses allocated frequency spectrum constraints, summarizes the international standardization process, and provides findings and recommendations from the world s first AeroMACS prototype implemented in Cleveland, Ohio, USA.

  9. A review of the Magnus effect in aeronautics

    Science.gov (United States)

    Seifert, Jost

    2012-11-01

    The Magnus effect is well-known for its influence on the flight path of a spinning ball. Besides ball games, the method of producing a lift force by spinning a body of revolution in cross-flow was not used in any kind of commercial application until the year 1924, when Anton Flettner invented and built the first rotor ship Buckau. This sailboat extracted its propulsive force from the airflow around two large rotating cylinders. It attracted attention wherever it was presented to the public and inspired scientists and engineers to use a rotating cylinder as a lifting device for aircraft. This article reviews the application of Magnus effect devices and concepts in aeronautics that have been investigated by various researchers and concludes with discussions on future challenges in their application.

  10. An Electronic Pressure Profile Display system for aeronautic test facilities

    Science.gov (United States)

    Woike, Mark R.

    1990-01-01

    The NASA Lewis Research Center has installed an Electronic Pressure Profile Display system. This system provides for the real-time display of pressure readings on high resolution graphics monitors. The Electronic Pressure Profile Display system will replace manometer banks currently used in aeronautic test facilities. The Electronic Pressure Profile Display system consists of an industrial type Digital Pressure Transmitter (DPI) unit which interfaces with a host computer. The host computer collects the pressure data from the DPI unit, converts it into engineering units, and displays the readings on a high resolution graphics monitor in bar graph format. Software was developed to accomplish the above tasks and also draw facility diagrams as background information on the displays. Data transfer between host computer and DPT unit is done with serial communications. Up to 64 channels are displayed with one second update time. This paper describes the system configuration, its features, and its advantages over existing systems.

  11. Applied simulation and optimization in logistics, industrial and aeronautical practice

    CERN Document Server

    Mota, Idalia; Serrano, Daniel

    2015-01-01

    Presenting techniques, case-studies and methodologies that combine the use of simulation approaches with optimization techniques for facing problems in manufacturing, logistics, or aeronautical problems, this book provides solutions to common industrial problems in several fields, which range from manufacturing to aviation problems, where the common denominator is the combination of simulation’s flexibility with optimization techniques’ robustness. Providing readers with a comprehensive guide to tackle similar issues in industrial environments, this text explores novel ways to face industrial problems through hybrid approaches (simulation-optimization) that benefit from the advantages of both paradigms, in order to give solutions to important problems in service industry, production processes, or supply chains, such as scheduling, routing problems and resource allocations, among others.

  12. Health monitoring of aeronautical structures based on vibrations measurements

    Science.gov (United States)

    Bovio, Igor; Lecce, Leonardo

    2006-03-01

    Purpose of the paper is to present an innovative application inside the Non Destructive Testing field based on vibrations measurements, developed by the authors during the last three years, and already tested for analysing damage of many structural elements. The proposed new method is based on the acquisition and comparison of Frequency Response Functions (FRFs) of the monitored structure before and after an occurred damage. Structural damage modify the dynamical behaviour of the structure such as mass, stiffened and damping, and consequently the FRFs of the damaged structure in comparison with the FRFs of the sound structure, making possible to identify, to localize and quantify a structural damage. The activities, presented in the paper, mostly focused on a new FRFs processing technique based on the determining of a representative "Damage Index" for identifying and analysing damage both on real scale aeronautical structural components, like large-scale fuselage reinforced panels, and on aeronautical composite panels. Besides it has been carried out a dedicated neural network algorithm aiming at obtaining a "recognition-based learning"; this kind of learning methodology permits to train the neural network in order to let it recognises only "positive" examples discarding as a consequence the "negative" ones. Within the structural NDT a "positive" example means "healthy" state of the analysed structural component and, obviously, a "negative" one means a "damaged" or perturbed state. From an architectural point of view piezoceramic patches have been tested as actuators and sensors. Besides it has been used a laser-scanning vibrometer system to validate the behaviour of the piezoceramic patches.

  13. NASA Ames Sustainability Initiatives: Aeronautics, Space Exploration, and Sustainable Futures

    Science.gov (United States)

    Grymes, Rosalind A.

    2015-01-01

    In support of the mission-specific challenges of aeronautics and space exploration, NASA Ames produces a wealth of research and technology advancements with significant relevance to larger issues of planetary sustainability. NASA research on NexGen airspace solutions and its development of autonomous and intelligent technologies will revolutionize both the nation's air transporation systems and have applicability to the low altitude flight economy and to both air and ground transporation, more generally. NASA's understanding of the Earth as a complex of integrated systems contributes to humanity's perception of the sustainability of our home planet. Research at NASA Ames on closed environment life support systems produces directly applicable lessons on energy, water, and resource management in ground-based infrastructure. Moreover, every NASA campus is a 'city'; including an urbanscape and a workplace including scientists, human relations specialists, plumbers, engineers, facility managers, construction trades, transportation managers, software developers, leaders, financial planners, technologists, electricians, students, accountants, and even lawyers. NASA is applying the lessons of our mission-related activities to our urbanscapes and infrastructure, and also anticipates a leadership role in developing future environments for living and working in space.

  14. Crack path in aeronautical titanium alloy under ultrasonic torsion loading

    Directory of Open Access Journals (Sweden)

    A. Nikitin

    2016-01-01

    Full Text Available This paper discusses features of fatigue crack initiation and growth in aeronautical VT3-1 titanium alloy under pure torsion loading in gigacycle regime. Two materials: extruded and forged VT3-1 titanium alloys were studied. Torsion fatigue tests were performed up to fatigue life of 109 cycles. The results of the torsion tests were compared with previously obtained results under fully reversed axial loading on the same alloys. It has been shown that independently on production process as surface as well subsurface crack initiation may appear under ultrasonic torsion loading despite the maximum stress amplitude located at the specimen surface. In the case of surface crack initiation, a scenario of crack initiation and growth is similar to HCF regime except an additional possibility for internal crack branching. In the case of subsurface crack, the initiation site is located below the specimen surface (about 200 μm and is not clearly related to any material flaw. Internal crack initiation is produced by shear stress in maximum shear plane and early crack growth is in Mode II. Crack branching is limited in the case of internal crack initiation compared to surface one. A typical ‘fish-eye’ crack can be observed at the torsion fracture surface, but mechanism of crack initiation seems not to be the same than under axial fatigue loading.

  15. An analysis of total quality management in Aeronautical Systems Division

    Science.gov (United States)

    Caudle, Mark D.

    1991-09-01

    This study investigated the major schools of thought on various aspects of quality management and quality improvement. Areas covered included definitions of waste and quality, views on the cost of quality, tools and techniques used for quality improvement, and management philosophies and frameworks for continuous improvement. In addition, this study analyzed the structure and training content of the current Total Quality Management program at Aeronautical Systems Division (ASD). Pre- and post-test surveys on employee attitudes toward organizational effectiveness were analyzed from the Advanced Cruise Missile System Program Office (SPO), the F-15 SPO, and the ASD Deputy Chief of Staff for Human Resources (ASD/DP). Data was supplemented with semi-structured, personal interviews with ASD personnel involved in TQM. Survey analysis showed that the ACM SPO significantly improved, ASD/DP significantly digressed, and the F-15 SPO remained basically consistent. This led to the conclusion that ASD allows too much flexibility in the implementation of TQM in the three-letter organizations.

  16. IPv6 Test Bed for Testing Aeronautical Applications

    Science.gov (United States)

    Wilkins, Ryan; Zernic, Michael; Dhas, Chris

    2004-01-01

    Aviation industries in United States and in Europe are undergoing a major paradigm shift in the introduction of new network technologies. In the US, NASA is also actively investigating the feasibility of IPv6 based networks for the aviation needs of the United States. In Europe, the Eurocontrol lead, Internet Protocol for Aviation Exchange (iPAX) Working Group is actively investigating the various ways of migrating the aviation authorities backbone infrastructure from X.25 based networks to an IPv6 based network. For the last 15 years, the global aviation community has pursued the development and implementation of an industry-specific set of communications standards known as the Aeronautical Telecommunications Network (ATN). These standards are now beginning to affect the emerging military Global Air Traffic Management (GATM) community as well as the commercial air transport community. Efforts are continuing to gain a full understanding of the differences and similarities between ATN and Internet architectures as related to Communications, Navigation, and Surveillance (CNS) infrastructure choices. This research paper describes the implementation of the IPv6 test bed at NASA GRC, and Computer Networks & Software, Inc. and these two test beds are interface to Eurocontrol over the IPv4 Internet. This research work looks into the possibility of providing QoS performance for Aviation application in an IPv6 network as is provided in an ATN based network. The test bed consists of three autonomous systems. The autonomous system represents CNS domain, NASA domain and a EUROCONTROL domain. The primary mode of connection between CNS IPv6 testbed and NASA and EUROCONTROL IPv6 testbed is initially a set of IPv6 over IPv4 tunnels. The aviation application under test (CPDLC) consists of two processes running on different IPv6 enabled machines.

  17. Sectoral Innovation Performance in the Space and Aeronautics Sectors. final report. Task 1

    NARCIS (Netherlands)

    Giessen, A.M. van der; Poel, M.

    2011-01-01

    The Space and Aeronautics Sectors are high tech manufacturing sectors. Between Space and Aeronautics Sectors are linkages and parallels. All major systems assemblers are active in both sectors. Examples are EADS but also Boeing, BAE Systems and manufacturers of propulsion systems and other component

  18. 78 FR 1848 - Plutonium-238 Production for Radioisotope Power Systems for National Aeronautics and Space...

    Science.gov (United States)

    2013-01-09

    ... Plutonium-238 Production for Radioisotope Power Systems for National Aeronautics and Space Administration...-238 (Pu-238) for radioisotope power systems (RPSs) to support the National Aeronautics and Space... Radioisotope Power Systems (Draft Consolidation EIS) in 2005 to consolidate the nuclear operations related...

  19. What kind of students should be developed through aeronautical engineering education?

    Science.gov (United States)

    Holloway, R. B.

    1975-01-01

    The educational requirements for future aeronautical engineering students are postulated. The change in aeronautical engineering from increasing aircraft performance without regard to cost is compared with the cost effective aspects of future research. The capabilities of future engineers are discussed with respect to the following areas: (1) problem solving, (2) planning and organizing, (3) communication, and (4) professionalism.

  20. 78 FR 41822 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-07-11

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... assurance that requires the property to be used for an aeronautical purpose. The property was acquired...

  1. 78 FR 63279 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-10-23

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... before modifying the land-use assurance that requires the property to be used for an aeronautical...

  2. 78 FR 59753 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-09-27

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... land-use assurance that requires the property to be used for an aeronautical purpose. The property...

  3. 78 FR 79059 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-12-27

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... assurance that requires the property to be used for an aeronautical purpose. The property was...

  4. 78 FR 22595 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-04-16

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... land-use assurance that requires the property to be used for an aeronautical purpose. The subject...

  5. 78 FR 41823 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-07-11

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... assurance that requires the property to be used for an aeronautical purpose. The two parcels proposed to...

  6. 78 FR 7816 - NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems Subcommittee Meeting

    Science.gov (United States)

    2013-02-04

    ... SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems... of the Aeronautics Committee of the NASA Advisory Council. The meeting will be held for the purpose..., Washington, DC 20546, (202) 358-1578, or brenda.l.mulac@nasa.gov . SUPPLEMENTARY INFORMATION: The...

  7. 77 FR 59020 - NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems Subcommittee; Meeting

    Science.gov (United States)

    2012-09-25

    ... SPACE ADMINISTRATION NASA Advisory Council; Aeronautics Committee; Unmanned Aircraft Systems... of the Aeronautics Committee of the NASA Advisory Council (NAC). The meeting will be held for the..., Washington, DC 20546, (202) 358-1578, or brenda.l.mulac@nasa.gov . SUPPLEMENTARY INFORMATION: The...

  8. National facilities study. Volume 2: Task group on aeronautical research and development facilities report

    Science.gov (United States)

    1994-01-01

    The Task Group on Aeronautics R&D Facilities examined the status and requirements for aeronautics facilities against the competitive need. Emphasis was placed on ground-based facilities for subsonic, supersonic and hypersonic aerodynamics, and propulsion. Subsonic and transonic wind tunnels were judged to be most critical and of highest priority. Results of the study are presented.

  9. The Aeronautics Education, Research, and Industry Alliance (AERIAL) 2002 Report. UNO Aviation Monograph Series. UNOAI Report.

    Science.gov (United States)

    Bowen, Brent D.; Box, Richard C.; Fink, Mary M.; Gogos, George; Lehrer, Henry R.; Narayanan, Ram M.; Nickerson, Jocelyn S.; O'Neil, Patrick D.; Tarry, Scott E.; Vlasek, Karisa D.

    This document contains four papers on aeronautics education, research, and partnerships that partly supported through the Aeronautics Education, Research, and Industry Alliance (AERIAL). The paper "2002 AERIAL Monograph" (Brent D. Bowen, Jocelyn S. Nickerson, Mary M. Fink, et al.) presents an overview of research and development in the…

  10. Aeronautics. An Educator's Guide with Activities in Science, Mathematics, and Technology Education: What Pilot, Astronaut, or Aeronautical Engineer didn't Start out with a Toy Glider?

    Science.gov (United States)

    Biggs, Pat (Editor); Huetter, Ted (Editor)

    1998-01-01

    Welcome to the exciting world of aeronautics. The term aeronautics originated in France, and was derived from the Greek words for "air" and "to sail." It is the study of flight and the operation of aircraft. This educator guide explains basic aeronautical concepts, provides a background in the history of aviation, and sets them within the context of the flight environment (atmosphere, airports, and navigation). The activities in this guide are designed to be uncomplicated and fun. They have been developed by NASA Aerospace Education Services Program specialists, who have successfully used them in countless workshops and student programs around the United States. The activities encourage students to explore the nature of flight, and experience some real-life applications of mathematics, science, and technology. The subject of flight has a wonderful power to inspire learning.

  11. Aeronautics and Space Report of the President: Fiscal Year 1996 Activities

    Science.gov (United States)

    1996-01-01

    Topics considered include: (1) Space launch activities: space shuttle missions; expendable launch vehicles. (2) Space science: astronomy and space physics; solar system exploration. (3) Space flight and technology: life and microgravity sciences; space shuttle technology; reuseable launch vehicles; international space station; energy; safety and mission assurance; commercial development and regulation of space; surveillance. (4) Space communications: communications satellites; space network; ground networks; mission control and data systems. (5) Aeronautical activities: technology developments; air traffic control and navigation; weather-related aeronautical activities; flight safety and security; aviation medicine and human factors. (6) Studies of the planet earth: terrestrial studies and applications: atmospheric studies: oceanographic studies; international aeronautical and space activities; and appendices.

  12. Exploration of Risks in Autonomous Decision-Making Applied to Aeronautics

    Data.gov (United States)

    National Aeronautics and Space Administration — Prior research into metrics and design for autonomy were presented. At this time, the prospect of adding significant autonomous decision-making on a piloted aircraft...

  13. Combustion/Emission Species Monitoring Ground and Flight Aeronautical Research Using a Gas Microsensor Array Project

    Data.gov (United States)

    National Aeronautics and Space Administration — The goal of this program is to develop a miniaturized and in-situ operated gas microsensor array for the real time monitoring of chemical composition of turbine...

  14. Combustion/Emission Species Monitoring Ground and Flight Aeronautical Research Using a Gas Microsensor Array Project

    Data.gov (United States)

    National Aeronautics and Space Administration — Makel Engineering, Inc. (MEI) and the Ohio State University (OSU) propose to develop high sensitivity, miniaturized and in-situ operated gas sensors for the real...

  15. 76 FR 50811 - Seventeenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security...

    Science.gov (United States)

    2011-08-16

    ... Federal Aviation Administration Seventeenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security (Joint Meeting) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION.... RTCA Specific Publication Progress and Update. WG--72. Introduction. Election of Secretary/Report...

  16. ICI Cancellation Algorithm for OFDM Based Aeronautical Communication Systems and Its Performance Analysis

    Institute of Scientific and Technical Information of China (English)

    AN Jian-ping; ZHANG De-sheng; WU Yan-bo

    2009-01-01

    d. We carried out Monte Carlo simulation with typical aeronautical en-route channel, and the simulation results are in agreement with the deduced theoretical performance expressions and validate the effect of our cancellation algorithm.

  17. Air Breathing Propulsion Controls and Diagnostics Research at NASA Glenn Under NASA Aeronautics Research Mission Programs

    Science.gov (United States)

    Garg, Sanjay

    2015-01-01

    The Intelligent Control and Autonomy Branch (ICA) at NASA (National Aeronautics and Space Administration) Glenn Research Center (GRC) in Cleveland, Ohio, is leading and participating in various projects in partnership with other organizations within GRC and across NASA, the U.S. aerospace industry, and academia to develop advanced controls and health management technologies that will help meet the goals of the NASA Aeronautics Research Mission Directorate (ARMD) Programs. These efforts are primarily under the various projects under the Advanced Air Vehicles Program (AAVP), Airspace Operations and Safety Program (AOSP) and Transformative Aeronautics Concepts Program (TAC). The ICA Branch is focused on advancing the state-of-the-art of aero-engine control and diagnostics technologies to help improve aviation safety, increase efficiency, and enable operation with reduced emissions. This paper describes the various ICA research efforts under the NASA Aeronautics Research Mission Programs with a summary of motivation, background, technical approach, and recent accomplishments for each of the research tasks.

  18. RFID Equivalent Model for Prediction of Functional and EMC Performances in Complex Aeronautic Environments

    Science.gov (United States)

    Piche, Alexandre; Perraud, Richard; Peres, Gilles; Nguyen, Francois; Herlem, Yannick

    2016-05-01

    Wireless networks are widely used in urban or office environments and are increasingly considered as an attractive solution for various aeronautic applications. Current investigations focus in particular on RFID technologies because of their widespread use, low cost and ease of installation. The objective of this publication is to propose a concept of RFID equivalent model to predict functional and EMC performances in complex aeronautic areas.

  19. 14 CFR 300.13 - Permanent disqualification of former Civil Aeronautics Board members and employees and DOT...

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Permanent disqualification of former Civil Aeronautics Board members and employees and DOT employees from matters in which they personally participated. 300.13 Section 300.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF...

  20. 77 FR 13173 - Notice of a Non-Aeronautical Land-Use Change Effecting the Quitclaim Deed and Federal Grant...

    Science.gov (United States)

    2012-03-05

    ... Federal Aviation Administration Notice of a Non-Aeronautical Land-Use Change Effecting the Quitclaim Deed... Administration, DOT. ACTION: Notice of a Non-aeronautical land-use change. SUMMARY: The Federal Aviation Administration (FAA) proposes to rule and invites public comment on the application for a non-aeronautical...

  1. 77 FR 40405 - Notice of a Non-Aeronautical Land-Use Change Effecting the Quitclaim Deed and Federal Grant...

    Science.gov (United States)

    2012-07-09

    ... Federal Aviation Administration Notice of a Non-Aeronautical Land-Use Change Effecting the Quitclaim Deed... Aviation Administration, DOT. ACTION: Notice of a Non-Aeronautical Land-Use Change. SUMMARY: The Federal...-aeronautical land- use change for approximately 38 acres of airport property at Delano Municipal...

  2. A Glimpse of Scientific Research on Fundamental Problems of Military and Civil Aeronautics

    Science.gov (United States)

    1939-01-01

    Among the outstanding accomplishments of the last century is man's conquest of the air. That conquest began in 1903 when the Wright brothers made the first successful flight of an airplane at Kitty Hawk, N. C. Five years later the United States Government purchased its first airplane for the use of the Army, and began the training of officers for military flying. During the years immediately preceding the outbreak of the World War the Government and a meager aircraft industry had made important progress, but the Government, practically the only customer, had purchased less than 100 airplanes. In the meantime, leading European nations, sensing acutely the potentialities of aircraft in warfare, had made greater progress and had begun laying the foundations for the new science of aeronautics. The World War gave a remarkable impetus to the development of aeronautics and emphasized the need for organized research on the fundamental problems of flight. By act of Congress approved March 3, 1915, the National Advisory Committee for Aeronautics was created and charged with the duty of supervising, directing, and conducting fundamental scientific research and experiment in aeronautics. With the farsighted support of the Congress the Committee has led the world in the development of unique aeronautical research facilities in its laboratories at Langley Field, Va. The research programs include problems initiated by the Committee and its subcommittees and also investigations requested by the Army, the Navy, and the Civil Aeronautics Authority. The results of researches conducted under one control, serve without duplication of effort, the needs of all branches of aviation, civil and military, and exert a profound influence on the progress of aeronautics by improving the performance, efficiency, and safety of aircraft. A brief description of the results of some of the committee's researches and of the equipment employed will be found in the following pages.

  3. An application of characteristic function in order to predict reliability and lifetime of aeronautical hardware

    Science.gov (United States)

    Żurek, Józef; Kaleta, Ryszard; Zieja, Mariusz

    2016-06-01

    The forecasting of reliability and life of aeronautical hardware requires recognition of many and various destructive processes that deteriorate the health/maintenance status thereof. The aging of technical components of aircraft as an armament system proves of outstanding significance to reliability and safety of the whole system. The aging process is usually induced by many and various factors, just to mention mechanical, biological, climatic, or chemical ones. The aging is an irreversible process and considerably affects (i.e. reduces) reliability and lifetime of aeronautical equipment. Application of the characteristic function of the aging process is suggested to predict reliability and lifetime of aeronautical hardware. An increment in values of diagnostic parameters is introduced to formulate then, using the characteristic function and after some rearrangements, the partial differential equation. An analytical dependence for the characteristic function of the aging process is a solution to this equation. With the inverse transformation applied, the density function of the aging of aeronautical hardware is found. Having found the density function, one can determine the aeronautical equipment's reliability and lifetime. The in-service collected or the life tests delivered data are used to attain this goal. Coefficients in this relationship are found using the likelihood function.

  4. Aeronautical Related Applications Using ATN and TCP/IP Research Report

    Science.gov (United States)

    Dhas, C.; Mulkerin, T.; Wargo, C.; Nielsen, R.; Gaughan, T.; Griner, James H., Jr. (Technical Monitor)

    2000-01-01

    The course for the future aeronautical communications architecture has been defined for more than 10 years and is known as the Aeronautical Telecommunication Network (ATN). However, the operational implementations of making use of the ATN remain 3-5 years away, and these implementations are still only in the early phases of long-range projects. Thus, it is an objective of this effort to consider what the potential outcome within the air transport industry may be, given the rapid growth in commercial-off-the-shelf (COTS) products, networks, and services that are based upon the Internet TCP/IP protocol suite.

  5. Aeronautics Research and Technology Program and specific objectives, fiscal year 1982

    Science.gov (United States)

    Olstad, W. B.

    1981-01-01

    The Aeronautics Research and Technology program is broken down into two program areas (research and technology base, and systems technology programs) which are further broken down into succeedingly more detailed activities to form a work breakdown structure for the aeronautics program: program area, program/discipline objective, specific objective, and research and technology objective and plan (RTOP). A detailed view of this work breakdown structure down to the specific objective level is provided, and goals or objectives at each of these levels are set forth. What is to be accomplished and why are addressed, but not how. The letter falls within the domain of the RTOP.

  6. Comparison of Marketing Techniques to Enroll Females at a Major Aeronautical University

    Science.gov (United States)

    Cross, David Scott

    2012-01-01

    Traditionally, industries belonging to the science, technology, engineering, and mathematics (STEM) fields are dominated by males. Recruitment and enrollment of females for STEM fields have become an issue among universities specializing in fields such as aviation and aeronautics. The research problem for this study was that marketing departments…

  7. 78 FR 19355 - Announcement of Charter Renewal of the Radio Technical Commission for Aeronautics (RTCA), Inc.

    Science.gov (United States)

    2013-03-29

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Announcement of Charter Renewal of the Radio Technical Commission for Aeronautics (RTCA), Inc. SUMMARY: The FAA is issuing this notice to advise the public of the charter...

  8. 78 FR 52841 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

    Science.gov (United States)

    2013-08-27

    ... Lockheed Martin Corporation/Lockheed Martin Aeronautics Company requested that we revise the NPRM (77 FR... other publications listed in this AD as of August 26, 2005 (70 FR 42262, July 22, 2005). ADDRESSES: For..., Amendment 39-14190 (70 FR 42262, July 22, 2005). AD 2005-15-01 applied to the specified products. The...

  9. [Toxological problems inherent in varnish and paint products used in aeronautics].

    Science.gov (United States)

    Cianetti, E; Bancheri, C

    1977-12-15

    Paint products and the need for their employment on aircraft and spacecraft are described and reference is made to the types of poisoning that may arise from their application. The main solvents and diluents are listed, together with their toxicological features. Lastly, mention is made of technical products required by the aeronautical regulations, the dangers associated with them, and the preventive measures required.

  10. 75 FR 80885 - Fifteenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security...

    Science.gov (United States)

    2010-12-23

    ... Federal Aviation Administration Fifteenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security (Joint Meeting) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of... PMC/ICC action on SC 216 TOR. Publication Progress and Update. Subgroup and Action Item...

  11. The predicament of aeronautical engineering education and what we can do about it

    Science.gov (United States)

    Bollard, R. J. H.

    1975-01-01

    Problems faced by the universities due to the drop in enrollment of aeronautics and astronautics undergraduate students are examined. Efforts made by the universities to overcome some of these problems are discussed. The author presents ten specific recommendations involving government and industry support to overcome the apparent lack of interest in engineering disciplines.

  12. 76 FR 41647 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model...

    Science.gov (United States)

    2011-07-15

    ... Register on January 5, 2011 (76 FR 485). That NPRM proposed to continue to require revising the maintenance... Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G Airplanes AGENCY... revising the FAA-approved maintenance program by incorporating new airworthiness limitations for fuel...

  13. 76 FR 485 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model...

    Science.gov (United States)

    2011-01-05

    ... System Design Review, Flammability Reduction and Maintenance and Inspection Requirements'' (66 FR 23086... Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G Airplanes AGENCY... revising the FAA- approved maintenance program by incorporating new airworthiness limitations for fuel...

  14. 78 FR 10248 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-02-13

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... be published in the Federal Register 30 days before modifying the land-use assurance that...

  15. 78 FR 73919 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-12-09

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance AGENCY... 30 days before modifying the land-use assurance that requires the property to be used for...

  16. 76 FR 34123 - 25th Meeting: RTCA Special Committee 206: Aeronautical Information and Meteorological Data Link

    Science.gov (United States)

    2011-06-10

    ... limited to space availability. With the approval of the chairmen, members of the public may present oral... issuing this notice to advise the public of a meeting of RTCA Special Committee 206: Aeronautical... with AEEC Systems Architecture & Interface SC 10 a.m. WG1, WG2, and WG3 Meetings 29 June--Wednesday 9...

  17. Graphene-Based Filters and Supercapacitors for Space and Aeronautical Applications

    Science.gov (United States)

    Calle, Carlos I.

    2015-01-01

    Overview of the capabilities of graphene for selective filters and for energy storage with a general description of the work being done at NASA Kennedy Space Center in collaboration with the University of California Los Angeles for space and aeronautical applications.

  18. A Portfolio Analysis Tool for Measuring NASAs Aeronautics Research Progress toward Planned Strategic Outcomes

    Science.gov (United States)

    Tahmasebi, Farhad; Pearce, Robert

    2016-01-01

    Description of a tool for portfolio analysis of NASA's Aeronautics research progress toward planned community strategic Outcomes is presented. The strategic planning process for determining the community Outcomes is also briefly described. Stakeholder buy-in, partnership performance, progress of supporting Technical Challenges, and enablement forecast are used as the criteria for evaluating progress toward Outcomes. A few illustrative examples are also presented.

  19. Achieving QoS for Aeronautical Telecommunication Networks over Differentiated Services

    Science.gov (United States)

    Bai, Haowei; Atiquzzaman, Mohammed; Ivancic, William

    2001-01-01

    Aeronautical Telecommunication Network (ATN) has been developed by the International Civil Aviation Organization to integrate Air-Ground and Ground-Ground data communication for aeronautical applications into a single network serving Air Traffic Control and Aeronautical Operational Communications. To carry time critical information required for aeronautical applications, ATN provides different Quality of Services (QoS) to applications. ATN has therefore, been designed as a standalone network which implies building an expensive separate network for ATN. However, the cost of operating ATN can be reduced if it can be run over a public network such as the Internet. Although the current Internet does not provide QoS, the next generation Internet is expected to provide QoS to applications. The objective of this paper is to investigate the possibility of providing QoS to ATN applications when it is run over the next generation Internet. Differentiated Services (DiffServ), one of the protocols proposed for the next generation Internet, will allow network service providers to offer different QoS to customers. Our results show that it is possible to provide QoS to ATN applications when they run over a DiffServ backbone.

  20. Quarterly Bulletin of the Division of Mechanical Engineering and the National Aeronautical Establishment, Ottawa, 1 April to 30 June, 1976.

    Science.gov (United States)

    EXPERIMENTAL DESIGN, PSYCHOMOTOR FUNCTION, CANADA, TEST METHODS, MODULES(ELECTRONICS), PATTERNS, MECHANICAL ENGINEERING , SYSTEMS ANALYSIS, HANDBOOKS, AERONAUTICAL ENGINEERING, SLEEP, FATIGUE(PHYSIOLOGY).

  1. Quarterly Bulletin of the Division of Mechanical Engineering and the National Aeronautical Establishment, Ottawa, 1 October to 31 December 1979.

    Science.gov (United States)

    1979-01-01

    Contents: NAE Convair 580 Aeromagnetics Program; Urban Traffic Signal Control for Fuel Economy; and Current Projects of the Division of Mechanical Engineering and the National Aeronautical Establishment.

  2. Quarterly Bulletin of the Division of Mechanical Engineering and the National Aeronautical Establishment, 1 October to 31 December 1975.

    Science.gov (United States)

    AERONAUTICS, * MECHANICAL ENGINEERING , SHIPS, CONTROL SYSTEMS, AIRCRAFT, CANADA, HUMAN FACTORS ENGINEERING, GAS DYNAMICS, MECHANICS, FUELS, ENGINES, MARINE ENGINEERING, HYDRODYNAMICS, HARBORS, AERODYNAMICS, FLIGHT RECORDERS.

  3. Quarterly Bulletin of the Division of Mechanical Engineering and the National Aeronautical Establishment, Ottawa, 1 July to 30 September 1978.

    Science.gov (United States)

    FOREIGN TECHNOLOGY, DATA PROCESSING, YAW, REAL TIME, SHOCK WAVES, CANADA, AERONAUTICS, MODEL TESTS, MECHANICAL ENGINEERING , GAS DISCHARGES, NAVAL ARCHITECTURE, HYDRODYNAMICS, SHOCK TUBES, LASER TRACKING, RAILROAD CARS.

  4. 14 CFR 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by...

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Maintenance, preventive maintenance, and... Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION § 43.17 Maintenance, preventive maintenance,...

  5. Aeronautical geographic data modeling based on GML%基于GML的航空地理数据建模

    Institute of Scientific and Technical Information of China (English)

    刘艳; 顾春艳

    2012-01-01

    Aeronautical information is an important type of geospatial data to ensure the safety and efficiency for air traffic. Currently, aeronautical information service (AIS) pro- vide these data to users by the medium of aeronautical chart, aeronautical information pub- lic (AIP), notice to airman (NOTA M), and so on. We are in the age of the Internet, sat- ellite navigation and computer networks, yet our approach to aeronautical geospatial data distribution is still based on paper charts, paper documentation and telex-based text mes- sages. Systems exist in isolation. Many of the data is entered more than twice in different computers using a keyboard rather than via file transfer or database transactions. To satisfy new requirements for the Global Air Traffic Management Operational Con- cept, aeronautical information services should be transferred to support a digital, real- time, accredited and secure aeronautical information environment. As an open geospatial data standard, GML gives aeronautical information feature coding method and interchan- ging format. Much has been done in air traffic community, and the technology has become more mature and is widely used. EUROCONTROL and FAA have developed AIXM (Aeronautical Information Exchange Model) based on GML. In Europe, the European AIS Database (EAD) provide unique reference database of aeronautical information on be- half of AIXM. In Chinese air traffic community, unique aeronautical geospatial data model has been considered as the key to ensure quality, integrity and interoperation of the aeronautical in- formation. But there is littlematerial progress on the data modeling. Based on studies on the characteristic of aeronautical information, the paper analyzed the mapping aeronautical data between and GML. Taking the basic aeronautical information database in Airline Management System as an example, an aeronautical geographic data model has been brought forward in this paper. Studies have shown that

  6. A method for the analysis of the benefits and costs for aeronautical research and technology

    Science.gov (United States)

    Williams, L. J.; Hoy, H. H.; Anderson, J. L.

    1978-01-01

    A relatively simple, consistent, and reasonable methodology for performing cost-benefit analyses which can be used to guide, justify, and explain investments in aeronautical research and technology is presented. The elements of this methodology (labeled ABC-ART for the Analysis of the Benefits and Costs of Aeronautical Research and Technology) include estimation of aircraft markets; manufacturer costs and return on investment versus aircraft price; airline costs and return on investment versus aircraft price and passenger yield; and potential system benefits--fuel savings, cost savings, and noise reduction. The application of this methodology is explained using the introduction of an advanced turboprop powered transport aircraft in the medium range market in 1978 as an example.

  7. A Novel Onboard-gateway-based Mechanism to Improve TCP Performance in Aeronautical Satellite Networks

    Institute of Scientific and Technical Information of China (English)

    2007-01-01

    The IP-based networks on aircraft serve to support Internet services via satellites. However, in aeronautical satellite hybrid networks, the TCP protocol performance often deteriorates due to improper decreases and slow recovery of the congestion window. This paper proposes a window size determination and notification mechanism, onboard-gateway-based mechanism (OGBM), which is based on the onboard gateway in the networks on aircraft. A cross-layer approach is adopted by the onboard gateway to obtain the satellite link bandwidth information. And then, by the gateway, through changing the receiver's advertised window field in ACK packets, TCP sources are notified of the window size of each TCP source calculated on the ground of bandwidth delay product and flow numbers. The mechanism is able to avoid improper changes of TCP window and serve multiple users. Simulation results show that the mechanism with the fairness index close to 1 improves TCP performance in aeronautical satellite networks.

  8. Achieving EMC Emissions Compliance for an Aeronautics Power Line Communications System

    Science.gov (United States)

    Dominiak, S.; Vos, G.; ter Meer, T.; Widmer, H.

    2012-05-01

    Transmitting data over the power distribution network - Power Line Communications (PLC) -provides an interesting solution to reducing the weight and complexity of wiring networks in commercial aircraft. One of the potential roadblocks for the introduction of this technology is achieving EMC emissions compliance. In this article an overview of the EMC conducted and radiated emissions testing for PLC- enabled aeronautics equipment is presented. Anomalies resulting from chamber resonances leading to discrepancies between the conducted emissions tests and the measured radiated emissions are identified and described. Measurements made according to the current version of the civil aeronautical EMC standard, EUROCAE ED-14F (RTCA DO-160F), show that PLC equipment can achieve full EMC emissions compliance.

  9. Analysis and design of over-current limit control strategies applied in aeronautical power supplies

    Institute of Scientific and Technical Information of China (English)

    WANG Lin-bing; HE Xiang-ning

    2007-01-01

    Some Over-Current Limit Control strategies are analyzed and designed to meet the demands of high reliability and rapid dynamic response in the aeronautical power supply applications. The control schemes are both effective in DC-DC converters and DC-AC converters. Controller models are set up, and the over-current limit operation principles of analogy and digital control are analyzed too. An 800VA aeronautical power supply has been constructed to verify the performance of the proposed control strategy in various cases such as the sudden load change and the constant load. The analysis and experiments confirm the advantages of the proposed over-current limit strategies as follows: simple,effective and reliable.

  10. Development of nonlinear acoustic propagation analysis tool toward realization of loud noise environment prediction in aeronautics

    Energy Technology Data Exchange (ETDEWEB)

    Kanamori, Masashi, E-mail: kanamori.masashi@jaxa.jp; Takahashi, Takashi, E-mail: takahashi.takashi@jaxa.jp; Aoyama, Takashi, E-mail: aoyama.takashi@jaxa.jp [Japan Aerospace Exploration Agency, 7-44-1, Jindaijihigashi-machi, Chofu, Tokyo (Japan)

    2015-10-28

    Shown in this paper is an introduction of a prediction tool for the propagation of loud noise with the application to the aeronautics in mind. The tool, named SPnoise, is based on HOWARD approach, which can express almost exact multidimensionality of the diffraction effect at the cost of back scattering. This paper argues, in particular, the prediction of the effect of atmospheric turbulence on sonic boom as one of the important issues in aeronautics. Thanks to the simple and efficient modeling of the atmospheric turbulence, SPnoise successfully re-creates the feature of the effect, which often emerges in the region just behind the front and rear shock waves in the sonic boom signature.

  11. Global mobile satellite communications theory for maritime, land and aeronautical applications

    CERN Document Server

    Ilčev, Stojče Dimov

    2017-01-01

    This book discusses current theory regarding global mobile satellite communications (GMSC) for maritime, land (road and rail), and aeronautical applications. It covers how these can enable connections between moving objects such as ships, road and rail vehicles and aircrafts on one hand, and on the other ground telecommunications subscribers through the medium of communications satellites, ground earth stations, Terrestrial Telecommunication Networks (TTN), Internet Service Providers (ISP) and other wireless and landline telecommunications providers. This new edition covers new developments and initiatives that have resulted in land and aeronautical applications and the introduction of new satellite constellations in non-geostationary orbits and projects of new hybrid satellite constellations. The book presents current GMSC trends, mobile system concepts and network architecture using a simple mode of style with understandable technical information, characteristics, graphics, illustrations and mathematics equ...

  12. On the Application of Time-Reversed Space-Time Block Code to Aeronautical Telemetry

    Science.gov (United States)

    2014-06-01

    impact of unequal power allocation in aeronautical telemetry channels. Two transmitting antennas are employed to exploit partial channel state... antennas are employed to exploit partial channel state information. GTR-STBC are observed to perform the best trade-off between the signal-to-noise ratio...Highly power-efficient transmitters, such as ra- dio frequency (RF) power amplifiers operating in full saturation , and constant-envelope modula- tion

  13. Profile of software engineering within the National Aeronautics and Space Administration (NASA)

    Science.gov (United States)

    Sinclair, Craig C.; Jeletic, Kellyann F.

    1994-01-01

    This paper presents findings of baselining activities being performed to characterize software practices within the National Aeronautics and Space Administration. It describes how such baseline findings might be used to focus software process improvement activities. Finally, based on the findings to date, it presents specific recommendations in focusing future NASA software process improvement efforts. The findings presented in this paper are based on data gathered and analyzed to date. As such, the quantitative data presented in this paper are preliminary in nature.

  14. Electrical conductivity improvement of aeronautical carbon fiber reinforced polyepoxy composites by insertion of carbon nanotubes

    OpenAIRE

    Lonjon, Antoine; Demont, Philippe; Dantras, Eric; Lacabanne, Colette

    2012-01-01

    International audience; An increase and homogenization of electrical conductivity is essential in epoxy carbon fiber laminar aeronautical composites. Dynamic conductivity measurements have shown a very poor transversal conductivity. Double wall carbon nanotubes have been introduced into the epoxy matrix to increase the electrical conductivity. The conductivity and the degree of dispersion of carbon nanotubes in epoxy matrix were evaluated. The epoxy matrix was filled with 0.4 wt.% of CNTs to ...

  15. Power Output and Air Requirements of a Two-stroke Cycle Engine for Aeronautical Use

    Science.gov (United States)

    Paton, C R; Kemper, Carlton

    1927-01-01

    This investigation was undertaken to determine the pressure and amount of air necessary for satisfactory high-speed, two-stroke cycle operation and thus permit the power requirements of the air pump or blower to be determined. Based on power output and air requirement here obtained the two-stroke cycle engine would seem to be favorable for aeronautical use. No attempts were made to secure satisfactory operation at idling speeds.

  16. CHINESE JOURNAL OF AERONAUTICS STARTS TO SET A WEBSITE FOR EACH OF ITS PUBLISHED PAPER

    Institute of Scientific and Technical Information of China (English)

    2000-01-01

    @@ In order to better meet the need of current scientific and technological community on information exchange, by taking advantage of the Internet, beginning from the first issue of the year 2000, Chinese Journal of Aeronautics (CJA) and Acta Aeronautica et Astronautica Sinica (AAAS) start to set a website for each of their published papers, which is referred to as "Article URL" and is typeset and printed at the lowest left corner of the footnote on the first page of that paper.

  17. Lessons Learned from Applying Design Thinking in a NASA Rapid Design Study in Aeronautics

    Science.gov (United States)

    McGowan, Anna-Maria; Bakula, Casey; Castner, Raymond

    2017-01-01

    In late 2015, NASA's Aeronautics Research Mission Directorate (ARMD) funded an experiment in rapid design and rapid teaming to explore new approaches to solving challenging design problems in aeronautics in an effort to cultivate and foster innovation. This report summarizes several lessons learned from the rapid design portion of the study. This effort entailed learning and applying design thinking, a human-centered design approach, to complete the conceptual design for an open-ended design challenge within six months. The design challenge focused on creating a capability to advance experimental testing of autonomous aeronautics systems, an area of great interest to NASA, the US government as a whole, and an entire ecosystem of users and developers around the globe. A team of nine civil servant researchers from three of NASA's aeronautics field centers with backgrounds in several disciplines was assembled and rapidly trained in design thinking under the guidance of the innovation and design firm IDEO. The design thinking process, while used extensively outside the aerospace industry, is less common and even counter to many practices within the aerospace industry. In this report, several contrasts between common aerospace research and development practices and design thinking are discussed, drawing upon the lessons learned from the NASA rapid design study. The lessons discussed included working towards a design solution without a set of detailed design requirements, which may not be practical or even feasible for management to ascertain for complex, challenging problems. This approach allowed for the possibility of redesigning the original problem statement to better meet the needs of the users. Another lesson learned was to approach problems holistically from the perspective of the needs of individuals that may be affected by advances in topic area instead of purely from a technological feasibility viewpoint. The interdisciplinary nature of the design team also

  18. Review and Preliminary Evaluation of Lifting Horizontal-Axis Rotating-Wing Aeronautical Systems (HARWAS)

    Science.gov (United States)

    ship propulsion and cycloidal ship propulsion . Approximately 1200 references are listed. A series of cross-index tables is also included to provide a quick means for the reader to determine the content and availability of the references. An analysis of the various lift systems pertinent to the HARWAS field is made with a view to potential air vehicle applications. Over 20 original aeronautical applications are identified and evaluated in the light of recent advances in power plants, transmissions and lightweight structural techniques. This analysis

  19. The NASA (National Aeronautics and Space Administration) Laboratory Telerobotic Manipulator control system architecture

    Energy Technology Data Exchange (ETDEWEB)

    Rowe, J.C.; Butler, P.L.; Glassell, R.L.; Herndon, J.N.

    1991-01-01

    In support of the National Aeronautics and Space Administration (NASA) goals to increase the utilization of dexterous robotic systems in space, the Oak Ridge National Laboratory (ORNL) has developed the Laboratory Telerobotic Manipulator (LTM) system. It is a dexterous, dual-arm, force reflecting teleoperator system with robotic features for NASA ground-based research. This paper describes the overall control system architecture, including both the hardware and software. The control system is a distributed, modular, and hierarchical design with flexible expansion capabilities for future enhancements of both the hardware and software. 6 refs., 4 figs.

  20. Integrated smart two-phase spreader to enhance reliability of power electronic modules in aeronautical applications

    Science.gov (United States)

    Mohaupt, Mikael; Barremaecker, Laurent; Wilson, Ian

    2014-07-01

    Reliability of power electronic modules is a key characteristic of existing and innovative modules. An increasing quantity of these modules is used in a large range of applications and addresses from annex up to vital functions, especially with the more electronic aircraft and recent developments in transport applications. To propose a solution to this lifetime issue, Microsemi and EHP have designed, manufactured and tested an improved flat heat pipe to fulfil aeronautic requirements. The frame of this development is based on the existing SP3 power module of Microsemi and significant decrease of thermal resistance is demonstrated by thermal tests.

  1. A Tool for Measuring NASA's Aeronautics Research Progress Toward Planned Strategic Community Outcomes

    Science.gov (United States)

    Tahmasebi, Farhad; Pearce, Robert

    2016-01-01

    Description of a tool for portfolio analysis of NASA's Aeronautics research progress toward planned community strategic Outcomes is presented. For efficiency and speed, the tool takes advantage of a function developed in Excels Visual Basic for Applications. The strategic planning process for determining the community Outcomes is also briefly discussed. Stakeholder buy-in, partnership performance, progress of supporting Technical Challenges, and enablement forecast are used as the criteria for evaluating progress toward Outcomes. A few illustrative examples of using the tool are also presented.

  2. NASA programs in advanced sensors and measurement technology for aeronautical applications

    Science.gov (United States)

    Conway, Bruce A.

    1990-01-01

    NASA involvement in the development, implementation, and experimental use of advanced aeronautical sensors and measurement technologies is presently discussed within the framework of specific NASA research centers' activities. The technology thrusts are in the fields of high temperature strain gages and microphones, laser light-sheet flow visualization, LTA, LDV, and LDA, tunable laser-based aviation meteorology, and fiber-optic CARS measurements. IR thermography and close-range photogrammetry are undergoing substantial updating and application. It is expected that 'smart' sensors will be increasingly widely used, especially in conjunction with smart structures in aircraft and spacecraft.

  3. 14 CFR 61.309 - What aeronautical knowledge must I have to apply for a sport pilot certificate?

    Science.gov (United States)

    2010-01-01

    ... and risk management. (l) Preflight actions that include— (1) How to get information on runway lengths... flight, windshear avoidance, and the procurement and use of aeronautical weather reports and...

  4. Remarks of Ruth Bates Harris, Deputy Assistant Administrator, National Aeronautics and Space Administration at summer institute closing activity

    Science.gov (United States)

    1975-01-01

    Applications of experience and knowledge gained from aeronautical and space research and exploration are discussed briefly. Spinoffs are presented which improve the quality of life by contributing to advances in health, transportation, foods, communications, energy, safety, and manufacturing.

  5. Aeronautics Education, Research, and Industry Alliance (AERIAL) Progress Report and Proposal for Funding Continuation NASA Nebraska EPSCoR

    Science.gov (United States)

    Bowen, Brent; Fink, Mary; Gogos, George; Moussavi, Massoum; Nickerson, Jocelyn; Rundquist, Donald; Russell, Valerie; Tarry, Scott

    2004-01-01

    The Aeronautics Education, Research, and Industry Alliance (AERIAL), which began as a comprehensive, multi-faceted NASA EPSCoR 2000 initiative, has contributed substantially to the strategic research and technology priorities of NASA, while intensifying Nebraska's rapidly growing aeronautics research and development endeavors. AERIAL has enabled Nebraska researchers to: (a) continue strengthening their collaborative relationships with NASA Field Centers, Codes, and Enterprises; (b) increase the capacity of higher education throughout Nebraska to invigorate and expand aeronautics research; and (c) expedite the development of aeronautics-related research infrastructure and industry in the state. Nebraska has placed emphasis on successfully securing additional funds from non-EPSCoR and non-NASA sources. AERIAL researchers have aggressively pursued additional funding opportunities offered by NASA, industry, and other agencies. This report contains a summary of AERIAL's activities and accomplishments during its first three years of implementation.

  6. Numerical prediction of heat affected layer in the EDM of aeronautical alloys

    Science.gov (United States)

    Izquierdo, B.; Plaza, S.; Sánchez, J. A.; Pombo, I.; Ortega, N.

    2012-10-01

    Electrical discharge machining is a popular non-traditional machining process, optimum for accurate machining of complex geometries in hard materials. EDM has been used for decades for machining pieces for the aeronautical industry, but surface integrity, and consequently the reliability of the machined parts have been questioned for long time due to the thermal nature of this machining process. In recent years, efforts have been put on modeling of the EDM process, being thermal modeling of the process one promising alternative. In a previous publication an original model of the EDM process was presented and it was used to predict material removal rate and surface finish for the EDM of steel. In the present article the capability of that modeling tool to characterize discharge properties and to predict recast layer distribution when EDMing an aeronautical alloy will be analyzed. EDM process of Inconel 718 has been studied and discharge properties have been obtained for four different EDM regimes. The capability of the model to reflect the behavior of more energetic regimes is discussed. Gathered information has been used to simulate the evolution of the recast layer generation process. Obtained results have been validated comparing them with experimental measurements, revealing a good correlation between predictions and experimental data. Finally, energetic efficiency of the discharge process has been simulated for the adjusted EDM regimes.

  7. Presentation of silicon platforms for wireless advanced networks of sensors for aeronautics application

    Science.gov (United States)

    Moreau, K.; Ruby, C.; Rolet, S.; Petitjean, B.; Rouet, V.

    2007-05-01

    The MEDEA+ SWANS (Silicon Platform for Wireless Advanced Networks of Sensors) project aims at defining a generic silicon platform, integrating analogue and digital Intellectual Property (IP) blocks for wireless sensor nodes technology. This generic platform will be used in various applications, such as transportation (aeronautics, automotive), homeland security, environmental and health/fitness. In the aeronautical application, the platform monitors, continuously, aircraft structures to detect whether a crack exists or not and process the data in real time, inside the platform. Measurements are provided by an inductive sensor glued on a structure and are acquired during flights. The sensor impedance (real and imaginary parts) varies depending on the state of the part area on which it is stuck. For example, this sensor aims at monitoring the further evolution of the crack too. The data are transmitted from the sensor to an ARM microcontroller through an electronic conditioner. Then, they are analysed and stored in a non volatile memory. Data measurements are collected by a RF transmission, every 2 or 4 months. A 3D stack platform demonstrator that allows the use of different technologies, will be realised, fully tested and characterised.

  8. Electromagnetic Compatibility Studies: LTE BS vs. Aeronautical Radionavigation Services in 694-790 MHz Frequency Band

    Directory of Open Access Journals (Sweden)

    Stankevičius Evaldas

    2014-10-01

    Full Text Available This paper presents the sharing analysis of the 694–790 MHz frequency band for Mobile services IMT and Aeronautical radio-navigation services (ARNS using SEAMCAT (established by CEPT software based on the statistical simulation (Monte-Carlo method. In 2012 the World Radiocommunication Conference (WRC-12 decided to allocate the 694–790 MHz frequency band (the so-called 700 MHz band to mobile services IMT (excluding aeronautical mobile after WRC-15 conference. But this agreement raises electromagnetic compatibility problems, which should be solved until WRC-15 [1]. This study was carried out in two phases: first applying theoretical analysis, then statistical Monte-Carlo simulations with SEAMCAT software tool in order to verify results obtained in theoretical approach. Analytical calculations shows that the required protection distances between ARNS stations and the MS base stations are 132 km. The obtained results from SEAMCAT simulations indicate that separation distance should be above 100 km. These results illustrate that the systems are not electromagnetically compatible. The possible mitigation technic could be antenna pattern correction.

  9. Aeronautics composite material inspection with a terahertz time-domain spectroscopy system

    Science.gov (United States)

    Ospald, Frank; Zouaghi, Wissem; Beigang, René; Matheis, Carsten; Jonuscheit, Joachim; Recur, Benoit; Guillet, Jean-Paul; Mounaix, Patrick; Vleugels, Wouter; Bosom, Pablo Venegas; González, Laura Vega; López, Ion; Edo, Rafael Martínez; Sternberg, Yehuda; Vandewal, Marijke

    2014-03-01

    The usability of pulsed broadband terahertz radiation for the inspection of composite materials from the aeronautics industry is investigated, with the goal of developing a mobile time-domain spectroscopy system that operates in reflection geometry. A wide range of samples based on glass and carbon fiber reinforced plastics with various types of defects is examined using an imaging system; the results are evaluated both in time and frequency domain. The conductivity of carbon fibers prevents penetration of the respective samples but also allows analysis of coatings from the reflected THz pulses. Glass fiber composites are, in principle, transparent for THz radiation, but commonly with significant absorption for wavelengths >1 THz. Depending on depth, matrix material, and size, defects like foreign material inserts, delaminations, or moisture contamination can be visualized. If a defect is not too deep in the sample, its location can be correctly identified from the delay between partial reflections at the surface and the defect itself.

  10. Assessment of Impact Detection Techniques for Aeronautical Application: ANN vs. LSSVM

    Science.gov (United States)

    Yue, N.; Sharif Khodaei, Z.

    2016-10-01

    The impact localization in composite panels is assessed using two machine learning techniques: least square support vector machines (LSSVM) and artificial neural networks (ANN) with local strain signals from piezoelectric sensors. Sensor signals from impact experiments on a composite plate as well as signals simulated by a finite element model are used to train and test models. A comparative study shows that LSSVM achieves better accuracy than ANN on identifying location of impacts for a combination of large mass impact and small mass impact, in particular when less data is available for training which is more appropriate for real aeronautical application. Additionally, LSSVM is more capable of identifying new impact events which have not been considered in the training process.

  11. Relay movement control for maintaining connectivity in aeronautical ad hoc networks

    Institute of Scientific and Technical Information of China (English)

    李杰; 孙志强; 师博浩; 宫二玲; 谢红卫

    2016-01-01

    As a new sort of mobile ad hoc network (MANET), aeronautical ad hoc network (AANET) has fleet-moving airborne nodes (ANs) and suffers from frequent network partitioning due to the rapid-changing topology. In this work, the additional relay nodes (RNs) is employed to repair the network and maintain connectivity in AANET. As ANs move, RNs need to move as well in order to re-establish the topology as quickly as possible. The network model and problem definition are firstly given, and then an online approach for RNs’ movement control is presented to make ANs achieve certain connectivity requirement during run time. By defining the minimum cost feasible moving matrix (MCFM), a fast algorithm is proposed for RNs’ movement control problem. Simulations demonstrate that the proposed algorithm outperforms other control approaches in the highly-dynamic environment and is of great potential to be applied in AANET.

  12. The impact of active controls technology on the structural integrity of aeronautical vehicles

    Science.gov (United States)

    Noll, Thomas E.; Austin, Edward; Donley, Shawn; Graham, George; Harris, Terry; Kaynes, Ian; Lee, Ben; Sparrow, James

    1993-01-01

    The findings of an investigation conducted under the auspices of The Technical Cooperation Program (TTCP) to assess the impact of active controls technology on the structural integrity of aeronautical vehicles and to evaluate the present state-of-the-art for predicting loads caused by a flight-control system modification and the resulting change in the fatigue life of the flight vehicle are summarized. Important points concerning structural technology considerations implicit in applying active controls technology in new aircraft are summarized. These points are well founded and based upon information received from within the aerospace industry and government laboratories, acquired by sponsoring workshops which brought together experts from contributing and interacting technical disciplines, and obtained by conducting a case study to independently assess the state of the technology. The paper concludes that communication between technical disciplines is absolutely essential in the design of future high performance aircraft.

  13. Structural damage detection in an aeronautical panel using analysis of variance

    Science.gov (United States)

    Gonsalez, Camila Gianini; da Silva, Samuel; Brennan, Michael J.; Lopes Junior, Vicente

    2015-02-01

    This paper describes a procedure for structural health assessment based on one-way analysis of variance (ANOVA) together with Tukey's multiple comparison test, to determine whether the results are statistically significant. The feature indices are obtained from electromechanical impedance measurements using piezoceramic sensor/actuator patches bonded to the structure. Compared to the classical approach based on a simple change of the observed signals, using for example root mean square responses, the decision procedure in this paper involves a rigorous statistical test. Experimental tests were carried out on an aeronautical panel in the laboratory to validate the approach. In order to include uncontrolled variability in the dynamic responses, the measurements were taken over several days in different environmental conditions using all eight sensor/actuator patches. The damage was simulated by controlling the tightness and looseness of the bolts and was correctly diagnosed. The paper discusses the strengths and weakness of the approach in light of the experimental results.

  14. Researches and studies regarding brazed aluminium alloys microstructure used in aeronautic industry

    Directory of Open Access Journals (Sweden)

    A. Dimitrescu

    2015-04-01

    Full Text Available Brazing is applied to the merge of the pieces which are most required, tensile strength of the solder can reach high values. By brazing there can be assembled pieces of most metals and ferrous and nonferrous alloys, with high melting temperature. This paper presents an analysis of the microstructure of materials from a brazed merge of aluminum alloy L103 which is often used to produce pieces of aeronautical industry. Brazing material was performed using several technologies, and after examination of the microstructure of materials from the merge area it was established as optimal technology the technology which consist of pickling in Aloclene 100 solution with the deposition of filler material on both sides of the base material and the use of spectral acetylene and neutral flame.

  15. Interference Analysis Status and Plans for Aeronautical Mobile Airport Communications System (AeroMACS)

    Science.gov (United States)

    Kerczewski, Robert J.; Wilson, Jeffrey D.

    2010-01-01

    Interference issues related to the operation of an aeronautical mobile airport communications system (AeroMACS) in the C-Band (specifically 5091-5150 MHz) is being investigated. The issue of primary interest is co-channel interference from AeroMACS into mobile-satellite system (MSS) feeder uplinks. The effort is focusing on establishing practical limits on AeroMACS transmissions from airports so that the threshold of interference into MSS is not exceeded. The analyses are being performed with the software package Visualyse Professional, developed by Transfinite Systems Limited. Results with omni-directional antennas and plans to extend the models to represent AeroMACS more accurately will be presented. These models should enable realistic analyses of emerging AeroMACS designs to be developed from NASA Test Bed, RTCA 223, and European results.

  16. Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences

    Directory of Open Access Journals (Sweden)

    Pablo Zuluaga-Ramírez

    2015-03-01

    Full Text Available We present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP, by measuring variations on the surface roughness. Variable amplitude loads (VAL, which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.

  17. Investigation of Surface Roughness in High-Speed Milling of Aeronautical Aluminum Alloy

    Institute of Scientific and Technical Information of China (English)

    PAN Yong-zhi; AI Xing; ZHAO Jun; WAN Yi

    2008-01-01

    An approach is presented to optimize the surface roughness in high-speed finish milling of 7050-T7451 aeronautical aluminum alloy. In view of this, the multi-linear regression model for surface roughness has been developed in terms of slenderness ratio, cutting speed, radial depth-of-cut and feed per tooth by means of orthogonal experimental design. Variance analyses were applied to check the adequacy of the predictive model and the significances of the independent input parameters. Response contours of surface roughness were generated by using response surface methodology (RSM). From these contours, it was possible to select an optimum combination of cutting parameters that improves machining efficiency without increasing the surface roughness.

  18. Role of Computational Fluid Dynamics and Wind Tunnels in Aeronautics R and D

    Science.gov (United States)

    Malik, Murjeeb R.; Bushnell, Dennis M.

    2012-01-01

    The purpose of this report is to investigate the status and future projections for the question of supplantation of wind tunnels by computation in design and to intuit the potential impact of computation approaches on wind-tunnel utilization all with an eye toward reducing the infrastructure cost at aeronautics R&D centers. Wind tunnels have been closing for myriad reasons, and such closings have reduced infrastructure costs. Further cost reductions are desired, and the work herein attempts to project which wind-tunnel capabilities can be replaced in the future and, if possible, the timing of such. If the possibility exists to project when a facility could be closed, then maintenance and other associated costs could be rescheduled accordingly (i.e., before the fact) to obtain an even greater infrastructure cost reduction.

  19. Concurrent Development and Certification of SOFTCOMAG 49AA Alloy for Aeronautical Applications

    Directory of Open Access Journals (Sweden)

    Ashok Kumar

    2012-01-01

    Full Text Available Softcomag 49AA alloy consisting of 49 wt per cent Fe, 49 wt. per cent Co and 2 wt per cent V is a soft magnetic alloy with a combination of very high saturation magnetisation and high magnetostriction and used for several aeronautical applications such as generators (stators and rotors, fixed iron moving armature units etc. Though this alloy is brittle in nature, it can be formed into hot rolled bars and cold rolled sheets by adopting suitable thermo mechanical treatments. In order to indigenise and subsequent type certification for aeronautical applications, the alloy was produced using 100 per cent virgin raw materials in a vacuum induction melting (VIM furnace which not only ensures substantial reduction of inclusions, but also the production of homogeneous alloy as a result of induction stirring. The chemical composition was examined and hot working parameters of the alloy were so optimised that they would result in the best combination of magnetic, physical and mechanical properties for the end use, which forms the central theme behind the developmental activity that was simultaneously covered by a comprehensive certification process. The material thus produced is subjected to stringent quality control checks in accordance with stipulated airworthiness norms. The paper discusses in detail the indigenisation efforts and airworthiness certification of the alloy Softcomag 49AA and its comparison with equivalent grades, namely PERMENDUR 49 and VACOFLUX 50.Defence Science Journal, 2012, 62(1, pp.67-72, DOI:http://dx.doi.org/10.14429/dsj.62.1093 

  20. Secure real-time wireless video streaming in the aeronautical telecommunications network

    Science.gov (United States)

    Czernik, Pawel; Olszyna, Jakub

    2010-09-01

    As Air Traffic Control Systems move from a voice only environment to one in which clearances are issued via data link, there is a risk that an unauthorized entity may attempt to masquerade as either the pilot or controller. In order to protect against this and related attacks, air-ground communications must be secured. The challenge is to add security in an environment in which bandwidth is limited. The Aeronautical Telecommunications Network (ATN) is an enabling digital network communications technology that addresses capacity and efficiency issues associated with current aeronautical voice communication systems. Equally important, the ATN facilitates migration to free flight, where direct computer-to-computer communication will automate air traffic management, minimize controller and pilot workload, and improve overall aircraft routing efficiency. Protecting ATN communications is critical since safety-of-flight is seriously affected if an unauthorized entity, a hacker for example, is able to penetrate an otherwise reliable communications system and accidentally or maliciously introduce erroneous information that jeopardizes the overall safety and integrity of a given airspace. However, an ATN security implementation must address the challenges associated with aircraft mobility, limited bandwidth communication channels, and uninterrupted operation across organizational and geopolitical boundaries. This paper provides a brief overview of the ATN, the ATN security concept, and begins a basic introduction to the relevant security concepts of security threats, security services and security mechanisms. Security mechanisms are further examined by presenting the fundamental building blocks of symmetric encipherment, asymmetric encipherment, and hash functions. The second part of this paper presents the project of cryptographiclly secure wireless communication between Unmanned Aerial Vehicles (UAV) and the ground station in the ATM system, based on the ARM9 processor

  1. Aeronautics Research Mission Directorate Integrated Systems Research Program (ISRP) and UAS Integration in the NAS Project

    Science.gov (United States)

    Wolfe, Jean

    2010-01-01

    Program Goal: Conduct research at an integrated system-level on promising concepts and technologies and explore, assess, or demonstrate the benefits in a relevant environment.Criteria for selection of projects for Integrated Systems Research: a) Technology has attained enough maturity in the foundational research program that they merit more in-depth evaluation at an integrated system level in a relevant environment. b) Technologies which systems analysis indicates have the most potential for contributing to the simultaneous attainment of goals. c) Technologies identified through stakeholder input as having potential for simultaneous attainment of goals. d) Research not being done by other government agencies and appropriate for NASA to conduct. e) Budget augmentation. Environmentally Responsible Aviation (ERA) Project Explore and assess new vehicle concepts and enabling technologies through system-level experimentation to simultaneously reduce fuel burn, noise, and emissions Unmanned Aircraft Systems (UAS) Integration in the National Airspace System (NAS) Project Contribute capabilities that reduce technical barriers related to the safety and operational challenges associated with enabling routine UAS access to the NAS Innovative Concepts for Green Aviation (ICGA) Project Spur innovation by offering research opportunities to the broader aeronautics community through peer-reviewed proposals, with a focus on making aviation more eco-friendly. Establish incentive prizes similar to the Centennial Challenges and sponsor innovation demonstrations of selected technologies that show promise of reducing aviation s impact on the environment

  2. Finite Element Simulation of Low Velocity Impact Damage on an Aeronautical Carbon Composite Structure

    Science.gov (United States)

    Lemanle Sanga, Roger Pierre; Garnier, Christian; Pantalé, Olivier

    2016-06-01

    Low velocity barely visible impact damage (BVID) in laminated carbon composite structures has a major importance for aeronautical industries. This contribution leads with the development of finite element models to simulate the initiation and the propagation of internal damage inside a carbon composite structure due by a low velocity impact. Composite plates made from liquid resin infusion process (LRI) have been subjected to low energy impacts (around 25 J) using a drop weight machine. In the experimental procedure, the internal damage is evaluated using an infrared thermographic camera while the indentation depth of the face is measured by optical measurement technique. In a first time we developed a robust model using homogenised shells based on degenerated tri-dimensional brick elements and in a second time we decided to modelize the whole stacking sequence of homogeneous layers and cohesive interlaminar interfaces in order to compare and validate the obtained results. Both layer and interface damage initiation and propagation models based on the Hashin and the Benzeggagh-Kenane criteria have been used for the numerical simulations. Comparison of numerical results and experiments has shown the accuracy of the proposed models.

  3. The American Institute of Aeronautics and Astronautics pre-college outreach program

    Science.gov (United States)

    Bering, E.; Bacon, L.; Copper, K.; Hansen, L. J.; Sanchez, M.; Aiaa Precollege Outreach Committee

    Throughout the United States school child perceive science technology engineering and mathematics STEM as difficult boring and often irrelevant subjects The possible reasons for this problem are endlessly debated however the economic social and overall national importance of producing graduates who are technically literate and enthusiastic in their support of a rational scientific world should motivate many scientific and engineering societies around the world to develop outreach programs aimed at children ages 5-18 and corresponding support programs aimed at schools and teachers covering kindergarten through 12 th grade The American Institute of Aeronautics and Astronautics AIAA is among those organizations that have identified the need to educate students and teachers about STEM current events and their direct affects on the United States population a way that motivates both to get more involved The AIAA has established a pre-college outreach program that has several major elements that will be described in this paper These elements include a pre-college Educator Associate Membership program a program to award small development grants to class room teachers and Educator of the Year awards and recognition program mechanisms for sharing and encouraging innovative local support programs and two national workshop events The first workshop event Passport to the Future is held annually in conjunction with the Joint Propulsion Conference It is intended to provide summertime training in Aerospace science education to classroom

  4. Fundamental Aeronautics Program: Overview of Propulsion Work in the Supersonic Cruise Efficiency Technical Challenge

    Science.gov (United States)

    Castner, Ray

    2012-01-01

    The Supersonics Project, part of NASA's Fundamental Aeronautics Program, contains a number of technical challenge areas which include sonic boom community response, airport noise, high altitude emissions, cruise efficiency, light weight durable engines/airframes, and integrated multi-discipline system design. This presentation provides an overview of the current (2012) activities in the supersonic cruise efficiency technical challenge, and is focused specifically on propulsion technologies. The intent is to develop and validate high-performance supersonic inlet and nozzle technologies. Additional work is planned for design and analysis tools for highly-integrated low-noise, low-boom applications. If successful, the payoffs include improved technologies and tools for optimized propulsion systems, propulsion technologies for a minimized sonic boom signature, and a balanced approach to meeting efficiency and community noise goals. In this propulsion area, the work is divided into advanced supersonic inlet concepts, advanced supersonic nozzle concepts, low fidelity computational tool development, high fidelity computational tools, and improved sensors and measurement capability. The current work in each area is summarized.

  5. Fundamental Aeronautics Program: Overview of Project Work in Supersonic Cruise Efficiency

    Science.gov (United States)

    Castner, Raymond

    2011-01-01

    The Supersonics Project, part of NASA?s Fundamental Aeronautics Program, contains a number of technical challenge areas which include sonic boom community response, airport noise, high altitude emissions, cruise efficiency, light weight durable engines/airframes, and integrated multi-discipline system design. This presentation provides an overview of the current (2011) activities in the supersonic cruise efficiency technical challenge, and is focused specifically on propulsion technologies. The intent is to develop and validate high-performance supersonic inlet and nozzle technologies. Additional work is planned for design and analysis tools for highly-integrated low-noise, low-boom applications. If successful, the payoffs include improved technologies and tools for optimized propulsion systems, propulsion technologies for a minimized sonic boom signature, and a balanced approach to meeting efficiency and community noise goals. In this propulsion area, the work is divided into advanced supersonic inlet concepts, advanced supersonic nozzle concepts, low fidelity computational tool development, high fidelity computational tools, and improved sensors and measurement capability. The current work in each area is summarized.

  6. Sandwich Structured Composites for Aeronautics: Methods of Manufacturing Affecting Some Mechanical Properties

    Directory of Open Access Journals (Sweden)

    Aneta Krzyżak

    2016-01-01

    Full Text Available Sandwich panels are composites which consist of two thin laminate outer skins and lightweight (e.g., honeycomb thick core structure. Owing to the core structure, such composites are distinguished by stiffness. Despite the thickness of the core, sandwich composites are light and have a relatively high flexural strength. These composites have a spatial structure, which affects good thermal insulator properties. Sandwich panels are used in aeronautics, road vehicles, ships, and civil engineering. The mechanical properties of these composites are directly dependent on the properties of sandwich components and method of manufacturing. The paper presents some aspects of technology and its influence on mechanical properties of sandwich structure polymer composites. The sandwiches described in the paper were made by three different methods: hand lay-up, press method, and autoclave use. The samples of sandwiches were tested for failure caused by impact load. Sandwiches prepared in the same way were used for structural analysis of adhesive layer between panels and core. The results of research showed that the method of manufacturing, more precisely the pressure while forming sandwich panels, influences some mechanical properties of sandwich structured polymer composites such as flexural strength, impact strength, and compressive strength.

  7. A comparison of Boolean-based retrieval to the WAIS system for retrieval of aeronautical information

    Science.gov (United States)

    Marchionini, Gary; Barlow, Diane

    1994-01-01

    An evaluation of an information retrieval system using a Boolean-based retrieval engine and inverted file architecture and WAIS, which uses a vector-based engine, was conducted. Four research questions in aeronautical engineering were used to retrieve sets of citations from the NASA Aerospace Database which was mounted on a WAIS server and available through Dialog File 108 which served as the Boolean-based system (BBS). High recall and high precision searches were done in the BBS and terse and verbose queries were used in the WAIS condition. Precision values for the WAIS searches were consistently above the precision values for high recall BBS searches and consistently below the precision values for high precision BBS searches. Terse WAIS queries gave somewhat better precision performance than verbose WAIS queries. In every case, a small number of relevant documents retrieved by one system were not retrieved by the other, indicating the incomplete nature of the results from either retrieval system. Relevant documents in the WAIS searches were found to be randomly distributed in the retrieved sets rather than distributed by ranks. Advantages and limitations of both types of systems are discussed.

  8. Designs that Fly: What the History of Aeronautics Tells Us about the Future of Design-Based Research in Education

    Science.gov (United States)

    O'Neill, D. Kevin

    2012-01-01

    For almost two decades, there has been growing interest in what design-based research (DBR) can contribute to both educational practice and theory. Since its introduction into the literature, this orientation to educational research has repeatedly been likened to aeronautical engineering as a way to clarify its nature and argue its potential. This…

  9. Funding and Strategic Alignment Guidance for Infusing Small Business Innovation Research Technology into Aeronautics Research Mission Directorate Projects for 2016

    Science.gov (United States)

    Nguyen, Hung D.; Steele, Gynelle C.

    2017-01-01

    This report is intended to help NASA program and project managers incorporate Small Business Innovation Research (SBIR) technologies into NASA Aeronautics Research Mission Directorate (ARMD) projects. Other Government and commercial project managers interested in ARMD funding opportunities through NASA's SBIR program will find this report useful as well.

  10. 77 FR 2605 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Gerald R. Ford International Airport...

    Science.gov (United States)

    2012-01-18

    ... authorize the lease of the airport property. The proposal consists of 2 parcels of land with the lease... compatible with local commercial/ industrial zoning classification. The land was acquired under the FAA... allowing the airport to lease the property, since the land is no longer needed for aeronautical...

  11. 77 FR 36602 - Public Notice for Waiver for Aeronautical Land-Use Assurance at Saline County Regional Airport...

    Science.gov (United States)

    2012-06-19

    ... Federal Aviation Administration Public Notice for Waiver for Aeronautical Land-Use Assurance at Saline... and 4th Street. The parcel was originally acquired as part of a donation to the County of Saline in...: Mr. Mark Westbrook, Airport Chairman, Saline County Regional Airport Commission, P.O. Box...

  12. 76 FR 36954 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Shell Lake Municipal Airport, Shell...

    Science.gov (United States)

    2011-06-23

    ... Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance; Shell Lake Municipal Airport, Shell Lake, WI AGENCY: Federal Aviation Administration, DOT ACTION: Notice of intent of... to authorize the release of 0.101 acres of the airport property at the ] Shell Lake Municipal...

  13. 77 FR 2603 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Willow Run Airport; Detroit, MI

    Science.gov (United States)

    2012-01-18

    ... Federal Aviation Administration Public Notice for Waiver of Aeronautical Land-Use Assurance; Willow Run... Willow Run Airport, Detroit, Michigan. SUPPLEMENTARY INFORMATION: Exhibit ``A'' Part of Section 12, Town... Easterly and Southerly line of the General Motors Corporation, Hydra-Matic Division, Willow Run...

  14. Budget estimates, fiscal year 1995. Volume 1: Agency summary, human space flight, and science, aeronautics and technology

    Science.gov (United States)

    1994-01-01

    The NASA budget request has been restructured in FY 1995 into four appropriations: human space flight; science, aeronautics, and technology; mission support; and inspector general. The human space flight appropriations provides funding for NASA's human space flight activities. This includes the on-orbit infrastructure (space station and Spacelab), transportation capability (space shuttle program, including operations, program support, and performance and safety upgrades), and the Russian cooperation program, which includes the flight activities associated with the cooperative research flights to the Russian Mir space station. These activities are funded in the following budget line items: space station, Russian cooperation, space shuttle, and payload utilization and operations. The science, aeronautics, and technology appropriations provides funding for the research and development activities of NASA. This includes funds to extend our knowledge of the earth, its space environment, and the universe and to invest in new technologies, particularly in aeronautics, to ensure the future competitiveness of the nation. These objectives are achieved through the following elements: space science, life and microgravity sciences and applications, mission to planet earth, aeronautical research and technology, advanced concepts and technology, launch services, mission communication services, and academic programs.

  15. Sources and Distribution of Polychlorinated Terphenyls at a Major US Aeronautics Research Facility.

    Science.gov (United States)

    HALE; ENOS; GALLAGHER

    1998-11-01

    / High concentrations of an unusual, complex mixture of chlorinated compounds were discovered in sediments and oysters near a federal aeronautics facility during implementation of a pollutant screening protocol. The mixture was identified as Aroclor 5432, a polychlorinated terphenyl (PCT) formulation, produced in the US until 1972. PCTs, particularly low chlorinated mixtures, have rarely been reported in the environment, despite significant manufacture and usage. Releases were traced to two outfalls. Creek sediments downstream of one contained concentrations as high as 200,000 |gmg/kg (dry weight basis); those in indigenous oysters reached 35,000 |gmg/kg, indicating significant bioavailability and bioaccumulation potential. Subsequent work showed that PCTs were widely disseminated in marsh grass, crabs, and fish. PCTs, PCBs, and mercury were also detected in storm drain lines entering these outfalls. The lines received input from both storm water and research buildings. Historical hydraulic fluid leaks and in-service compressor fluids in some buildings contained PCTs and PCBs. Contaminated materials on-site were removed to minimize pollutant spread. Aroclor 5432 usage, most likely as compressor/hydraulic fluid additives, probably ended about ten years prior to its on-site detection. In terms of biological effects, intraperitoneal injection of fish with Aroclor 5432 induced cytochrome P-4501A (CYP1A) and ethoxyresorufin O-deethylase (EROD) activity to a similar degree as PCB Aroclor 1254 and to a greater extent than PCT Aroclor 5460. The presence of high concentrations of PCTs contributed to the facility being included on the National Priorities List. It subsequently became the first US federal facility to sign a Federal Facility Agreement, identifying cleanup responsibilities, prior to formal listing.KEY WORDS: Polychlorinated terphenyls; Aroclor; Contaminated sediments; Hydraulic fluid; Enzyme induction; Polychlorinated biphenyls

  16. Safety Risk Knowledge Elicitation in Support of Aeronautical R and D Portfolio Management: A Case Study

    Science.gov (United States)

    Shih, Ann T.; Ancel, Ersin; Jones, Sharon Monica; Reveley, Mary S.; Luxhoj, James T.

    2012-01-01

    Aviation is a problem domain characterized by a high level of system complexity and uncertainty. Safety risk analysis in such a domain is especially challenging given the multitude of operations and diverse stakeholders. The Federal Aviation Administration (FAA) projects that by 2025 air traffic will increase by more than 50 percent with 1.1 billion passengers a year and more than 85,000 flights every 24 hours contributing to further delays and congestion in the sky (Circelli, 2011). This increased system complexity necessitates the application of structured safety risk analysis methods to understand and eliminate where possible, reduce, and/or mitigate risk factors. The use of expert judgments for probabilistic safety analysis in such a complex domain is necessary especially when evaluating the projected impact of future technologies, capabilities, and procedures for which current operational data may be scarce. Management of an R&D product portfolio in such a dynamic domain needs a systematic process to elicit these expert judgments, process modeling results, perform sensitivity analyses, and efficiently communicate the modeling results to decision makers. In this paper a case study focusing on the application of an R&D portfolio of aeronautical products intended to mitigate aircraft Loss of Control (LOC) accidents is presented. In particular, the knowledge elicitation process with three subject matter experts who contributed to the safety risk model is emphasized. The application and refinement of a verbal-numerical scale for conditional probability elicitation in a Bayesian Belief Network (BBN) is discussed. The preliminary findings from this initial step of a three-part elicitation are important to project management practitioners as they illustrate the vital contribution of systematic knowledge elicitation in complex domains.

  17. Research and Development Progress of National Key Laboratory of Advanced Composites on Advanced Aeronautical Resin Matrix Composites

    Directory of Open Access Journals (Sweden)

    LI Bintai

    2016-06-01

    Full Text Available Applications and research progress in advanced aeronautical resin matrix composites by National Key Laboratory of Advanced Composites (LAC were summarized. A novel interlaminar toughening technology employing ultra-thin TP non-woven fabric was developed in LAC, which significantly improved the compression after impact (CAI performances of composite laminates.Newly designed multilayer sandwich stealth composite structures exhibited a good broadband radar absorbing properties at 1-18 GHz.There were remarkable developments in high toughness and high temperature resin matrix composites, covering major composite processing technologies such as prepreg-autoclave procedure, liquid composite molding and automation manufacture, etc. Finally, numerical simulation and optimization methods were deliberately utilized in the study of composites curing behavior, resin flow and curing deformation. A composite material database was also established.In conclusion, LAC has been a great support for the development of aeronautical equipment, playing such roles as innovation leading, system dominating, foundation supporting and application ensuring of aerocomposites.

  18. Lean Purchasing Management of Aeronautical Manufacture Enterprise%航空制造企业精益采购管理

    Institute of Scientific and Technical Information of China (English)

    李云鹤

    2011-01-01

    This paper analyzed the purchasing management aeronautical manufactures enterprise, and studied the new status and challenges in the theory of lean supply and Lean production. A novel purchasing management mode of aeronautical manufactures enterprise is proposed, adopts the purchasing planning, contract management, and achieve the lean management of purchasing process. This paper designs the lean purchasing management system, which include purchasing planning, contract management, order tracing, vendor evaluation platform and so on. Finally, the proposed system is applied in an aeronautical manufactures enterprise.%分析了航空制造企业供应采购管理现状,研究了精益生产、精益供应理论下数字化采购管理面临的问题和挑战,提出了符合现代航空制造特点的数字化采购管理模式,以采购计划、采购合同为核心,实现了采购全过程精益管理;设计了数字化采购管理系统系统,涵盖了计划采购、合同管理、订单跟踪以及供应商评价等主要功能,系统在某大型航空制造企业得到应用,实现了预期应用目标.

  19. Contributions to understanding the high speed machining effects on aeronautic part surface integrity

    Science.gov (United States)

    Jomaa, Walid

    To remain competitive, the aeronautic industry has increasing requirements for mechanical components and parts with high functional performance and longer in-service life. The improvement of the in-service life of components can be achieved by mastering and optimizing the surface integrity of the manufactured parts. Thus, the present study attempted to investigate, experimentally and theoretically, the tool/work material interactions on part surface integrity during the machining of aluminium alloys and hardened materials (low alloy steels) using orthogonal machining tests data. The studied materials are two aluminum alloys (6061-T6 and 7075-T651) and AISI 4340 steel. The AISI 4340 steel was machined after been induction heat treated to 58-60 HRC. These materials were selected in an attempt to provide a comprehensive study for the machining of metals with different behaviours (ductile and hard material). The proposed approach is built on three steps. First, we proposed a design of experiment (DOE) to analyse, experimentally, the chip formation and the resulting surface integrity during the high speed machining under dry condition. The orthogonal cutting mode, adopted in these experiments, allowed to explore, theoretically, the effects of technological (cutting speed and feed) and physical (cutting forces, temperature, shear angle, friction angle, and length Contact tool/chip) parameters on the chip formation mechanisms and the machined surface characteristics (residual stress, plastic deformation, phase transformation, etc.). The cutting conditions were chosen while maintaining a central composite design (CCD) with two factors (cutting speed and feed per revolution). For the aluminum 7075-T651, the results showed that the formation of BUE and the interaction between the tool edge and the iron-rich intermetallic particles are the main causes of the machined surface damage. The BUE formation increases with the cutting feed while the increase of the cutting speed

  20. Report by A.Berson about the aerological expedition of the Royal Aeronautic Observatory to East Africa in 1908

    Directory of Open Access Journals (Sweden)

    R. Süring

    2013-07-01

    Full Text Available This paper is the edited translation of the paper “A. Berson's Bericht über die aerologische Expedition des königlichen aeronautischen Observatoriums nach Ostafrika im Jahre 1908” (Report by A. Berson about the aerological expedition of the Royal Aeronautic Observatory to East Africa in 1908 that was published 1910 in the Meteorologische Zeitschrift 27, 536–542. The paper, provided by R. Süring, co-editor of the journal, is a summary of a more extensive report published in the same year.

  1. Investigation of an expert health monitoring system for aeronautical structures based on pattern recognition and acousto-ultrasonics

    Science.gov (United States)

    Tibaduiza-Burgos, Diego Alexander; Torres-Arredondo, Miguel Angel

    2015-08-01

    Aeronautical structures are subjected to damage during their service raising the necessity for periodic inspection and maintenance of their components so that structural integrity and safe operation can be guaranteed. Cost reduction related to minimizing the out-of-service time of the aircraft, together with the advantages offered by real-time and safe-life service monitoring, have led to a boom in the design of inexpensive and structurally integrated transducer networks comprising actuators, sensors, signal processing units and controllers. These kinds of automated systems are normally referred to as smart structures and offer a multitude of new solutions to engineering problems and multi-functional capabilities. It is thus expected that structural health monitoring (SHM) systems will become one of the leading technologies for assessing and assuring the structural integrity of future aircraft. This study is devoted to the development and experimental investigation of an SHM methodology for the detection of damage in real scale complex aeronautical structures. The work focuses on each aspect of the SHM system and highlights the potentialities of the health monitoring technique based on acousto-ultrasonics and data-driven modelling within the concepts of sensor data fusion, feature extraction and pattern recognition. The methodology is experimentally demonstrated on an aircraft skin panel and fuselage panel for which several damage scenarios are analysed. The detection performance in both structures is quantified and presented.

  2. 19th Biannual Symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR)

    CERN Document Server

    Heller, Gerd; Krämer, Ewald; Wagner, Claus; Breitsamter, Christian

    2016-01-01

    This book presents contributions to the 19th biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. Though the book’s primary emphasis is on the aerospace context, it also addresses further important applications, e.g. in ground transportation and energy. .

  3. The National Aeronautics and Space Administration's Earth Science Applications Program: Exploring Partnerships to Enhance Decision Making in Public Health Practice

    Science.gov (United States)

    Vann, Timi S.; Venezia, Robert A.

    2002-01-01

    The National Aeronautics and Space Administration (NASA), Earth Science Enterprise is engaged in applications of NASA Earth science and remote sensing technologies for public health. Efforts are focused on establishing partnerships with those agencies and organizations that have responsibility for protecting the Nation's Health. The program's goal is the integration of NASA's advanced data and technology for enhanced decision support in the areas of disease surveillance and environmental health. A focused applications program, based on understanding partner issues and requirements, has the potential to significantly contribute to more informed decision making in public health practice. This paper intends to provide background information on NASA's investment in public health and is a call for partnership with the larger practice community.

  4. Modeling, Analysis and Simulation Approaches Used in Development of the National Aeronautics and Space Administration Max Launch Abort System

    Science.gov (United States)

    Yuchnovicz, Daniel E.; Dennehy, Cornelius J.; Schuster, David M.

    2011-01-01

    The National Aeronautics and Space Administration (NASA) Engineering and Safety Center was chartered to develop an alternate launch abort system (LAS) as risk mitigation for the Orion Project. Its successful flight test provided data for the design of future LAS vehicles. Design of the flight test vehicle (FTV) and pad abort trajectory relied heavily on modeling and simulation including computational fluid dynamics for vehicle aero modeling, 6-degree-of-freedom kinematics models for flight trajectory modeling, and 3-degree-of-freedom kinematics models for parachute force modeling. This paper highlights the simulation techniques and the interaction between the aerodynamics, flight mechanics, and aerodynamic decelerator disciplines during development of the Max Launch Abort System FTV.

  5. Analysis of atmospheric flow over a surface protrusion using the turbulence kinetic energy equation with reference to aeronautical operating systems

    Science.gov (United States)

    Frost, W.; Harper, W. L.

    1975-01-01

    Flow over surface obstructions can produce significantly large wind shears such that adverse flying conditions can occur for aeronautical systems (helicopters, STOL vehicles, etc.). Atmospheric flow fields resulting from a semi-elliptical surface obstruction in an otherwise horizontally homogeneous statistically stationary flow are modelled with the boundary-layer/Boussinesq-approximation of the governing equation of fluid mechanics. The turbulence kinetic energy equation is used to determine the dissipative effects of turbulent shear on the mean flow. Iso-lines of turbulence kinetic energy and turbulence intensity are plotted in the plane of the flow and highlight regions of high turbulence intensity in the stagnation zone and sharp gradients in intensity along the transition from adverse to favourable pressure gradient. Discussion of the effects of the disturbed wind field in CTOL and STOL aircraft flight path and obstruction clearance standards is given. The results indicate that closer inspection of these presently recommended standards as influenced by wind over irregular terrains is required.

  6. An Overview of the NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Ultra High Bypass Partnership Research Goals

    Science.gov (United States)

    Hughes, Christopher E.

    2009-01-01

    An overview of the NASA Fundamental Aeronautics Program (FAP) mission and goals is presented. One of the subprograms under the FAP, the Subsonic Fixed Wing Project (SFW), is the focus of the presentation. The SFW system environmental metrics are discussed, along with highlights of planned, systematic approach to research to reduce the environmental impact of commercial aircraft in the areas of acoustics, fuel burn and emissions. The presentation then focuses on collaborative research being conducted with U.S. Industry on the Ultra High Bypass (UHB) engine cycle, the propulsion cycle selected by the SFW to meet the system goals. The partnerships with General Electric Aviation to investigate Open Rotor propulsion concepts and with Pratt & Whitney to investigate the Geared Turbofan UHB engine are highlighted, including current and planned future collaborative research activities with NASA and each organization.

  7. In-flight simulators and fly-by-wirelight demonstrators a historical account of international aeronautical research

    CERN Document Server

    2017-01-01

    This book offers the first complete account of more than sixty years of international research on In-Flight Simulation and related development of electronic and electro-optic flight control system technologies (“Fly-by-Wire” and “Fly-by-Light”). They have provided a versatile and experimental procedure that is of particular importance for verification, optimization, and evaluation of flying qualities and flight safety of manned or unmanned aircraft systems. Extensive coverage is given in the book to both fundamental information related to flight testing and state-of-the-art advances in the design and implementation of electronic and electro-optic flight control systems, which have made In-Flight Simulation possible. Written by experts, the respective chapters clearly show the interdependence between various aeronautical disciplines and in-flight simulation methods. Taken together, they form a truly multidisciplinary book that addresses the needs of not just flight test engineers, but also other aerona...

  8. Evolutionary optimization and game strategies for advanced multi-disciplinary design applications to aeronautics and UAV design

    CERN Document Server

    Periaux, Jacques; Lee, Dong Seop Chris

    2015-01-01

    Many complex aeronautical design problems can be formulated with efficient multi-objective evolutionary optimization methods and game strategies. This book describes the role of advanced innovative evolution tools in the solution, or the set of solutions of single or multi disciplinary optimization. These tools use the concept of multi-population, asynchronous parallelization and hierarchical topology which allows different models including precise, intermediate and approximate models with each node belonging to the different hierarchical layer handled by a different Evolutionary Algorithm. The efficiency of evolutionary algorithms for both single and multi-objective optimization problems are significantly improved by the coupling of EAs with games and in particular by a new dynamic methodology named “Hybridized Nash-Pareto games”. Multi objective Optimization techniques and robust design problems taking into account uncertainties are introduced and explained in detail. Several applications dealing with c...

  9. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1987, volume 2

    Science.gov (United States)

    Jones, William B., Jr. (Editor); Goldstein, Stanley H. (Editor)

    1987-01-01

    The 1987 Johnson Space Center (JCS) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship program was conducted by Texas A and M University and JSC. The 10-week program was operated under the auspices of ASEE. The basic objectives of the program are: to further the professional knowledge of qualified engineering and science faculty members; to stimulate an exchange of ideas between participants and NASA; to enrich and refresh the research and teaching activities of participants' institutions; and to contribute to the research objective of the NASA Centers. This document is a compilation of the final reports on the research projects done by the faculty fellows during the summer of 1987.

  10. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1992, volume 1

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Goldstein, Stanley H. (Editor)

    1992-01-01

    The 1992 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, Washington, DC. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objective of the NASA Centers. This document is a compilation of the final reports 1 through 12.

  11. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program 1988, volume 2

    Science.gov (United States)

    Bannerot, Richard B.; Goldstein, Stanley H.

    1989-01-01

    The 1988 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by the University of Houston and JCS. The 10-week program was operated under the auspices of the ASEE. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters, Washington, D.C. The objectives of the program, which began in 1965 at JSC and in 1964 nationally, are: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objectives of the NASA Centers.

  12. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program 1988, volume 1

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Goldstein, Stanley H. (Editor)

    1989-01-01

    The 1988 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The 10-week program was operated under the auspices of the ASEE. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters, Washington, D.C. The objectives of the program, which began in 1965 at JSC and in 1964 nationally, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objectives of the NASA Centers.

  13. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1992, volume 2

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Goldstein, Stanley H. (Editor)

    1992-01-01

    The 1992 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters Washington, DC. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objective of the NASA Centers. This document contains reports 13 through 24.

  14. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1989, volume 2

    Science.gov (United States)

    Jones, William B., Jr. (Editor); Goldstein, Stanley H. (Editor)

    1989-01-01

    The 1989 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by Texas A and M University and JSC. The 10-week program was operated under the auspices of the ASEE. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters, Washington, D.C. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objective of the NASA Centers.

  15. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1989, volume 1

    Science.gov (United States)

    Jones, William B., Jr. (Editor); Goldstein, Stanley H. (Editor)

    1989-01-01

    The 1989 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by Texas A and M University and JSC. The 10-week program was operated under the auspices of the ASEE. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters, Washington, D.C. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objective of the NASA Centers.

  16. The Relationship of a Pilot's Educational Background, Aeronautical Experience and Recency of Experience to Performance In Initial Training at a Regional Airline

    Science.gov (United States)

    Shane, Nancy R.

    The purpose of this study was to determine how a pilot's educational background, aeronautical experience and recency of experience relate to their performance during initial training at a regional airline. Results show that variables in pilots' educational background, aeronautical experience and recency of experience do predict performance in training. The most significant predictors include years since graduation from college, multi-engine time, total time and whether or not a pilot had military flying experience. Due to the pilot shortage, the pilots entering regional airline training classes since August 2013 have varied backgrounds, aeronautical experience and recency of experience. As explained by Edward Thorndike's law of exercise and the law of recency, pilots who are actively using their aeronautical knowledge and exercising their flying skills should exhibit strong performance in those areas and pilots who have not been actively using their aeronautical knowledge and exercising their flying skills should exhibit degraded performance in those areas. Through correlation, chi-square and multiple regression analysis, this study tests this theory as it relates to performance in initial training at a regional airline.

  17. Application of MAC protocol in aeronautical Ad Hoc networks%MAC协议在航空自组网中应用综述

    Institute of Scientific and Technical Information of China (English)

    曹振林; 孙荣平; 柏长帅

    2013-01-01

      MAC protocol of aeronautical Ad hoc network is a direct controller of grouping messages in the wireless channel sending and reception. Therefore,in aeronautical Ad Hoc network,it is crucial for the performance of aeronautical Ad Hoc net⁃work whether MAC protocol can efficiently and fairly use the limited wireless channel resources. The MAC functions and the in⁃fluence factors of aeronautical Ad Hoc networks on MAC protocols are summarized in in this paper. MAC protocol characteristics of the wireless Ad Hoc networks and the key technologys of aeronautical Ad Hoc networks are analyzed in combination with the application of MAC in MANET.%  航空自组网MAC协议是分组报文在无线信道上发送和接收的直接控制者,因此,在航空自组网中,MAC协议能否高效、公平地利用有限的无线信道资源对航空自组网的性能起至关重要的作用。概述了MAC的功能作用、航空自组网对MAC协议的影响因素,并结合MAC在MANET中的应用,分析了无线自组网MAC协议的特点和航空自组网MAC协议的关键技术。

  18. A network design of military aeronautical communication based on MANET%一种基于MANET的军事航空通信网络设计

    Institute of Scientific and Technical Information of China (English)

    管伟; 任清华; 熊金石; 郑博

    2011-01-01

    在MANET研究中,网络拓扑结构对网络性能有直接影响.军事航空通信的特殊性决定了航空网络结构的特殊性.提出了一种航空自组网拓扑结构模型,并给出了基于OFDM的MAC协议思想,同时提出了一种分区层次路由协议.%In the research of MANET, the topology of the network directly detennines the performance of network. The particularity of military aeronautical communication detennines the particularity of aeronautical network structure. The article presents a topology structure model of the aeronautical Ad Hoc network and shows an idea of MAC protocol based on OFDM. At the same time, it suggests a divisional hierarchy routing protocol.

  19. [NASA/DOD Aerospace Knowledge Diffusion Research Project. Report 1, part 2:] Technical communications in aeronautics: Results of an exploratory study

    Science.gov (United States)

    Pinelli, Thomas E.; Glassman, Myron; Oliu, Walter E.; Barclay, Rebecca O.

    1989-01-01

    A study was undertaken that explored several aspects of technical communications in aeronautics. The study, which utilized survey research in the form of a self-administered questionnaire, was sent to 2,000 randomly selected members of the American Institute of Aeronautics and Astronautics. Six hundred and six usable questionnaires (30.3 percent) were received by the established cut off date. Part 2 of this study lists appendices to part 1, including survey instrument, aggregate totals, cross tabulations, and open-ended comments.

  20. Journal of Aeronautics.

    Science.gov (United States)

    1982-07-21

    Dislocation Structures of 2024 Aluminum Alloy, by Li Qingsheng, Tsai Chikung , Chen Xianxi, Pan Tian- xi...AND FATIGUE DISLOCATION STRUCTURES OF 2024 ALUMINUM ALLOY Li Qingsheng, Tsai Chikung , Chen Xianxi, Pan Tianxi Central Iron and Steel Research Institute...express our thanks.. Reference Literature 1) Tsai Chikung , Jin Shu Xue Bao, 1976 Nian 12 Juan 1 Qi 45 Ye. "Tsai Chikung , Journal of Metals, Vol. 12

  1. Lightning in aeronautics

    Science.gov (United States)

    Lago, F.

    2014-11-01

    It is generally accepted that a civilian aircraft is struck, on average, once or twice per year. This number tends to indicate that a lightning strike risk is far from being marginal and so requires that aircraft manufacturers have to demonstrate that their aircraft is protected against lightning. The first generation of aircrafts, which were manufactured mainly in aluminium alloy and had electromechanical and pneumatic controls, had a natural immunity to the effects of lightning. Nowadays, aircraft structures are made primarily with composite materials and flight controls are mostly electronic. This aspect of the "more composite and more electric" aircraft demands to aircraft manufacturers to pay a particular attention to the lightning protection and to its certification by testing and/or analysis. It is therefore essential to take this risk into account when designing the aircraft. Nevertheless, it is currently impossible to reproduce the entire lightning phenomenon in testing laboratories and the best way to analyse the lightning protection is to reproduce its effects. In this context, a number of standards and guides are produced by standards committees to help laboratories and aircraft manufacturers to perform realistic tests. Although the environment of a laboratory is quite different from those of a storm cloud, the rules of aircraft design, the know-how of aircraft manufacturers, the existence of international work leading to a better understanding of the lightning phenomenon and standards more precise, permit, today, to consider the risk as properly controlled.

  2. Aeronautical Materials (Selected Articles),

    Science.gov (United States)

    1984-03-13

    is necessary to make a brief evaluation of the studies on the micromorphology and mechanical behavior of initial period fatigue crack propagation as...proposed. See Reference [2] for details. As regards the micromorphology of the initial period of fatigue crack propagation, in their observations of

  3. The past, present, and future of National Aeronautics and Space Administration spaceflight diet in support of microgravity rodent experiments.

    Science.gov (United States)

    Sun, Gwo-Shing; Tou, Janet C; Yu, Diane; Girten, Beverly E; Cohen, Jacob

    2014-02-01

    Rodents have been the most frequently flown animal model used to study physiological responses to the space environment. In support of future of space exploration, the National Aeronautics and Space Administration (NASA) envisions an animal research program focused on rodents. Therefore, the development of a rodent diet that is suitable for the spaceflight environment including long duration spaceflight is a high priority. Recognizing the importance of nutrition in affecting spaceflight physiological responses and ensuring reliable biomedical and biological science return, NASA developed the nutrient-upgraded rodent food bar (NuRFB) as a standard diet for rodent spaceflight. Depending on future animal habitat hardware and planned spaceflight experiments, modification of the NuRFB or development of a new diet formulation may be needed, particularly for long term spaceflights. Research in this area consists primarily of internal technical reports that are not readily accessible. Therefore, the aims of this contribution are to provide a brief history of the development of rodent spaceflight diets, to review the present diet used in rodent spaceflight studies, and to discuss some of the challenges and potential solutions for diets to be used in future long-term rodent spaceflight studies.

  4. National Aeronautics and Space Administration (NASA)/American Society of Engineering Education (ASEE) Summer Faculty Fellowship Program - 2000

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Sickorez, Donn G. (Editor)

    2003-01-01

    The 2000 Johnson Space Center (JSC) National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The 10-week program was operated under the auspices of the ASEE. The program at JSC, as well as the programs at other NASA Centers, was funded by the Office of University Affairs, NASA Headquarters, Washington, D.C. The objectives of the program, which began in 1965 at JSC and 1964 nationally, are to (1) further the professional knowledge of qualified engineering and science faculty, (2) stimulate an exchange of ideas between participants and NASA, (3) enrich and refresh the research and teaching activities of participants' institutions, and (4) contribute to the research objectives of the NASA Centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project commensurate with her/his interests and background, and worked in collabroation with a NASA/JSC colleague. This document is a compilation of the final reports on the research projects done by the faculty fellows during the summer of 2000.

  5. Natural Atmospheric Environment Model Development for the National Aeronautics and Space Administration's Second Generation Reusable Launch Vehicle

    Science.gov (United States)

    Roberts, Barry C.; Leahy, Frank; Overbey, Glenn; Batts, Glen W.; Parker, Nelson (Technical Monitor)

    2002-01-01

    The National Aeronautics and Space Administration (NASA) recently began development of a new reusable launch vehicle. The program office is located at Marshall Space Flight Center (MSFC) and is called the Second Generation Reusable Launch Vehicle (2GRLV). The purpose of the program is to improve upon the safety and reliability of the first generation reusable launch vehicle, the Space Shuttle. Specifically, the goals are to reduce the risk of crew loss to less than 1-in-10,000 missions and decreased costs by a factor of 10 to approximately $1,000 per pound of payload launched to low Earth orbit. The program is currently in the very early stages of development and many two-stage vehicle concepts will be evaluated. Risk reduction activities are also taking place. These activities include developing new technologies and advancing current technologies to be used by the vehicle. The Environments Group at MSFC is tasked by the 2GRLV Program to develop and maintain an extensive series of analytical tools and environmental databases which enable it to provide detailed atmospheric studies in support of structural, guidance, navigation and control, and operation of the 2GRLV.

  6. Hazard-evaluation and technical-assistance report HETA 89-276-l2093, Lockheed Aeronautical Systems Company, Marietta, Georgia

    Energy Technology Data Exchange (ETDEWEB)

    Salisbury, S.; Bernard, B.P.; Wilcox, T.; Gunter, B.

    1991-01-01

    In response to a request from the International Association of Machinists and Aerospace Workers, NIOSH conducted an evaluation at the Lockheed Aeronautical Systems Company, Marietta, Georgia due to concerns about health hazards from exposure to epoxy and polyurethane paints being sprayed in open areas on the C-130 aircraft assembly line. About 350 employees worked on the final assembly line. Air samples were collected to evaluate potential exposures to diisocyanates, organic vapors, and trace metals released during painting operations. Environmental sampling demonstrated minimal risk of exposure for nonpainters to organic vapors, isocyanate prepolymers, and toxic metals released into the open atmosphere during first shift painting of wing panels. Area monitors showed airborne concentrations of organic vapors and hazardous particulates which were below current occupational limits. Exposure risks to hexavalent chromium (7440473) compounds were shown for one of the painters spraying primer containing strontium-chromate (7789062). The large interior volume of the building and the rapid dispersion and upward drift of paint overspray may tend to reduce the chance of floor level exposures. The practice of spraying polyurethane when the building was mostly unoccupied should prevent new cases of respiratory sensitization to diisocyanates among the C-130 production workers. The authors recommend specific measures to reduce exposures to diisocyanates and hexavalent chromium compounds.

  7. Funding and Strategic Alignment Guidance for Infusing Small Business Innovation Research Technology Into Aeronautics Research Mission Directorate Programs and Projects for 2015

    Science.gov (United States)

    Nguyen, Hung D.; Steele, Gynelle C.

    2016-01-01

    This report is intended to help NASA program and project managers incorporate Small Business Innovation Research/Small Business Technology Transfer (SBIR)/(STTR) technologies into NASA Aeronautics Research Mission Directorate (ARMD) projects. Other Government and commercial projects managers can also find this useful.

  8. Funding and Strategic Alignment Guidance for Infusing Small Business Innovation Research Technology into NASA Programs Associated with the Aeronautics Research Mission Directorate

    Science.gov (United States)

    Nguyen, Hung D.; Steele, Gynelle C.

    2015-01-01

    This report is intended to help NASA program and project managers incorporate Small Business Innovation Research/Small Business Technology Transfer (SBIR/STTR) technologies that have gone through Phase II of the SBIR program into NASA Aeronautics and Mission Directorate (ARMD) programs. Other Government and commercial program managers can also find this information useful.

  9. Design-Build-Write: Increasing the Impact of English for Specific Purposes Learning and Teaching in Aeronautical Engineering Education through Multiple Intelligences Task Design

    Science.gov (United States)

    Tatzl, Dietmar

    2011-01-01

    This article presents an English for Specific Purposes (ESP) task developed for teaching aeronautical engineering students. The task Design-Build-Write rests on the assumption that engineering students are skilled at mathematical reasoning, problem solving, drawing and constructing. In Gardner's 1983 Multiple Intelligences (MI) theory, these…

  10. 14 CFR 61.407 - What aeronautical knowledge must I have to apply for a flight instructor certificate with a sport...

    Science.gov (United States)

    2010-01-01

    ... apply for a flight instructor certificate with a sport pilot rating? 61.407 Section 61.407 Aeronautics... CERTIFICATION: PILOTS, FLIGHT INSTRUCTORS, AND GROUND INSTRUCTORS Flight Instructors With a Sport Pilot Rating... sport pilot rating? (a) Except as specified in paragraph (c) of this section you must receive and...

  11. [NASA/DOD Aerospace Knowledge Diffusion Research Project. Report 1, part 1:] Technical communications in aeronautics: Results of an exploratory study

    Science.gov (United States)

    Pinelli, Thomas E.; Glassman, Myron; Oliu, Walter E.; Barclay, Rebecca O.

    1989-01-01

    A study was undertaken that explored several aspects of technical communications in aeronautics. The study, which utilized survey research in the form of a self-administered questionnaire, was sent to 2,000 randomly selected members of the American Institute of Aeronautics and Astronautics. Six hundred and six usable questionnaires (30.3 percent) were received by the established cut off date. The study had five objectives. The first was to solicit the opinions of aeronautical engineers and scientists regarding the importance of technical communications to their profession; second, to determine their use and production of technical communications; third, to seek their views on the content of an undergraduate course in technical communications; fourth, to determine their use of libraries/technical information centers; and finally, to determine the use and importance of computer and information technology to them. The findings add considerable information to the knowledge of technical communications practices among aeronautical engineers and scientists and reinforce some of the conventional wisdom about technical communications and question other widely-held notions.

  12. Dynamic Strain Measurements on Automotive and Aeronautic Composite Components by Means of Embedded Fiber Bragg Grating Sensors.

    Science.gov (United States)

    Lamberti, Alfredo; Chiesura, Gabriele; Luyckx, Geert; Degrieck, Joris; Kaufmann, Markus; Vanlanduit, Steve

    2015-10-26

    The measurement of the internal deformations occurring in real-life composite components is a very challenging task, especially for those components that are rather difficult to access. Optical fiber sensors can overcome such a problem, since they can be embedded in the composite materials and serve as in situ sensors. In this article, embedded optical fiber Bragg grating (FBG) sensors are used to analyze the vibration characteristics of two real-life composite components. The first component is a carbon fiber-reinforced polymer automotive control arm; the second is a glass fiber-reinforced polymer aeronautic hinge arm. The modal parameters of both components were estimated by processing the FBG signals with two interrogation techniques: the maximum detection and fast phase correlation algorithms were employed for the demodulation of the FBG signals; the Peak-Picking and PolyMax techniques were instead used for the parameter estimation. To validate the FBG outcomes, reference measurements were performed by means of a laser Doppler vibrometer. Sensors 2015, 15 27175 The analysis of the results showed that the FBG sensing capabilities were enhanced when the recently-introduced fast phase correlation algorithm was combined with the state-of-the-art PolyMax estimator curve fitting method. In this case, the FBGs provided the most accurate results, i.e. it was possible to fully characterize the vibration behavior of both composite components. When using more traditional interrogation algorithms (maximum detection) and modal parameter estimation techniques (Peak-Picking), some of the modes were not successfully identified.

  13. Dynamic Strain Measurements on Automotive and Aeronautic Composite Components by Means of Embedded Fiber Bragg Grating Sensors

    Directory of Open Access Journals (Sweden)

    Alfredo Lamberti

    2015-10-01

    Full Text Available The measurement of the internal deformations occurring in real-life composite components is a very challenging task, especially for those components that are rather difficult to access. Optical fiber sensors can overcome such a problem, since they can be embedded in the composite materials and serve as in situ sensors. In this article, embedded optical fiber Bragg grating (FBG sensors are used to analyze the vibration characteristics of two real-life composite components. The first component is a carbon fiber-reinforced polymer automotive control arm; the second is a glass fiber-reinforced polymer aeronautic hinge arm. The modal parameters of both components were estimated by processing the FBG signals with two interrogation techniques: the maximum detection and fast phase correlation algorithms were employed for the demodulation of the FBG signals; the Peak-Picking and PolyMax techniques were instead used for the parameter estimation. To validate the FBG outcomes, reference measurements were performed by means of a laser Doppler vibrometer. Sensors 2015, 15 27175 The analysis of the results showed that the FBG sensing capabilities were enhanced when the recently-introduced fast phase correlation algorithm was combined with the state-of-the-art PolyMax estimator curve fitting method. In this case, the FBGs provided the most accurate results, i.e. it was possible to fully characterize the vibration behavior of both composite components. When using more traditional interrogation algorithms (maximum detection and modal parameter estimation techniques (Peak-Picking, some of the modes were not successfully identified.

  14. Biochemical analysis of the Hormoconis resinae fungal mycelium in the corrosion of aeronautical aluminium alloys

    Directory of Open Access Journals (Sweden)

    Araya, R.

    2007-06-01

    Full Text Available Biochemical analyses of the Hormoconis resinae fungal mycelium would explain behaviour differences of corrosive and non-corrosive strains on Al and its aeronautical alloys. In previous works its aggressiveness had been studied through SEM-EDX surface analysis, electrochemical techniques and immersion testing. In this paper separation of the proteins of the mycelium produced by a non-corrosive strain and its culture along three generations was performed. Cultures were prepared in batch in the presence and absence of pure Al and AA 2024, AA 7005 and AA 7075 alloys. The mycelia grown throughout the three generations increasingly
    recovered usual characteristics at the third replication, included their corrosiveness on Al and its alloys previously shown by all our strains. Amongst the bio-molecule fractions isolated and analysed during this preliminary study only the proteins revealed changes with the generation grown. When this fungal strain was cultured in the presence of alloy metal sheets electrophoresis of the protean fraction was correlative with the distinct mycelia behaviour observed, including corrosiveness on Al and its alloys.

    Las diferencias entre el comportamiento corrosivo y no corrosivo de una cepa del hongo Hormoconis resinae sobre aluminio y sus aleaciones aeronáuticas se explicarían a través de análisis bioquímicos del micelio. En trabajos previos, el comportamiento corrosivo se estudió mediante análisis de superficie SEM-EDX, técnicas electroquímicas y ensayos de inmersión. En este trabajo, se llevó a cabo la separación de proteínas del micelio producido por una cepa que perdió su corrosividad y su cultivo a través de tres generaciones. Cultivos en batch, en presencia y ausencia de aluminio y sus aleaciones AA 2024, AA 7005 y AA 7075, a través de tres generaciones del micelio crecido, fueron recuperando sus características, incluida su habitual corrosividad, en la tercera replicaci

  15. Description of an aeronautical geometry conversion package: Wave-drag to Langley Wireframe Geometry Standard (LaWGS) to Supersonic Implicit Marching Potential (SIMP)

    Science.gov (United States)

    Wiese, Michael R.

    1987-01-01

    Documented is an aeronautical geometry conversion package which translates wave-drag geometry into the Langley Wireframe Geometry Standard (LaWGS) format and then into a format which is used by the Supersonic Implicit Marching Potential (SIMP) program. The programs described were developed by Computer Sciences Corporation for the Advanced Vehicles Division/Advanced Concepts Branch at NASA Langley Research Center. Included also are the input and output from a benchmark test case.

  16. Effects of Be, Sr, Fe and Mg interactions on the microstructure and mechanical properties of aluminum based aeronautical alloys

    Science.gov (United States)

    Ibrahim, Mohamed Fawzy

    The present work was carried out on a series of heat-treatable aluminum-based aeronautical alloys containing various amounts of magnesium (Mg), iron (Fe), strontium (Sr) and beryllium (Be). Tensile test bars (dendrite arm spacing ~ 24mum) were solutionized for either 5 or 12 hours at 540°C, followed by quenching in warm water (60°C). Subsequently, these quenched samples were aged at 160°C for times up to 12 hours. Microstructural assessment was performed. All heat-treated samples were pulled to fracture at room temperature using a servo-hydraulic tensile testing machine. The results show that Be causes partial modification of the eutectic silicon (Si) particles similar to that reported for Mg addition. Addition of 0.8 wt.% Mg reduced the eutectic temperature by ~10°C. During solidification of alloys containing high levels of Fe and Mg, without Sr, a peak corresponding to the formation of a Be-Fe phase (Al8Fe2BeSi) was detected at 611°C. The Be-Fe phase precipitates in a script-like morphology. A new quinary eutectic-like reaction was observed to take place near the end of solidification of high Mg, high Fe, Be-containing alloys. This new reaction is composed mainly of fine particles of Si, Mg2Si, pi-Al 8Mg3FeSi6 and (Be-Fe) phases. The volume fraction of this reaction decreased with the addition of Sr. The addition of Be has a noticeable effect on decreasing the beta-phase length, or volume fraction, this effect may be limited by adding Sr. Beryllium addition also results in the precipitation of the beta-phase in a nodular form, which reduces the harmful effects of these intermetallics on the alloy mechanical properties. Increasing both Mg and Fe levels led to an increase in the amount of the pi-phase; increasing the iron content led to an increase in the volume fraction of the partially soluble beta- and pi-phases, while Mg2Si particles were completely dissolved. The beta-phase platelets were observed to undergo changes in their morphology due to the

  17. Instantaneous characteristics simulation and analysis on three-level brushless AC synchronous generators of aeronautic constant speed and frequency AC power system

    Science.gov (United States)

    Ma, Xiaohe; Shen, Songhua

    2006-11-01

    This paper mainly introduces theoretical analysis and experimental results of instantaneous characteristics on a certain three level brushless three-phase AC synchronous generators. The analysis, modeling and simulations with Simplorer software of Ansoft Company are carried out. It establishes three level generator models, gives theoretical relation matrix equation, and simulates some instantaneous characteristics. Design of the system requires reliable simulation tools with comprehensive component libraries capable of dealing with complex system behavior. The simulation results verify that the proposed system model can efficiently simulate the instantaneous characteristics of the real AC generator system. It gives better design experiences and digital methods for aeronautic constant speed and frequency AC power system.

  18. Quality Management Principles as Illustrated by the Organization of Romanian Inter-War Factories. A Century of Romanian Industrial Tradition in Aeronautics

    Directory of Open Access Journals (Sweden)

    Manuela RUSU

    2017-03-01

    Full Text Available Inter-war Romania developed 6 aircraft factories, the first starting its activity in 1916. Four of these, with three located in Bucharest, produced over 2000 aircraft, maily for the military use as Romania entered the Second World War. The activity of these factories was undertaken in times when nobody thought about formulating the principles of quality management and the research of the first scientists in quality, Deming, Shewhart and Juran had not yet been accepted or published. The work aims to present the inter-war Romanian aeronautical industry developments regarding the quality management.

  19. Funding and Strategic Alignment Guidance for Infusing Small Business Innovation Research Technology Into Aeronautics Research Mission Directorate Projects at NASA Glenn Research Center for 2015

    Science.gov (United States)

    Nguyen, Hung D.; Steele, Gynelle C.; Morris, Jessica R.

    2015-01-01

    This document is intended to enable the more effective transition of NASA Glenn Research Center (GRC) SBIR technologies funded by the Small Business Innovation Research (SBIR) program as well as its companion, the Small Business Technology Transfer (STTR) program into NASA Aeronautics Research Mission Directorate (ARMD) projects. Primarily, it is intended to help NASA program and project managers find useful technologies that have undergone extensive research and development (RRD), through Phase II of the SBIR program; however, it can also assist non-NASA agencies and commercial companies in this process. aviation safety, unmanned aircraft, ground and flight test technique, low emissions, quiet performance, rotorcraft

  20. Information Fusion in Supportability Assessment of Aeronautic Equipment%航空装备保障性评价中的信息融合技术

    Institute of Scientific and Technical Information of China (English)

    王强; 刘雪峰; 端木京顺

    2001-01-01

    Supportability assessment is an important job in the AeronauticEquipment's entire life cycle and it is a certification of the working effect of Integrated Logistics Support of aeronautic equipment. But in the supportability assessment of the aeronautic equipment, there are such problems as the redundancy of information, an unnecessarily wide range of time and space scope, and a lack of accuracy. With the first ever introduction of information fusion in supportability assessment and the analysis of the suitability of information fusion in supportability assessment, this paper researches into the rules and fusion models of information fusion in supportability assessment and puts forward a brand-new strategy model of supportability information fusion. So, this paper has practical value in improving the accuracy of aeronautic equipment supportability assessment results and in pushing on the development of supportability assessment.%航空装备保障性评价是航空装备寿命周期过程中的一项重要工作,是对航空装备开展综合保障工作效果的验证,但航空装备保障性评价中往往存在信息量大、时空覆盖范围广、准确性不高的问题。因此文中首次将信息融合技术引入保障性评价工作,分析了信息融合技术在保障性评价中的适用性,探索了信息融合技术在保障性评价中的准则及融合模型,提出了全新的保障性信息融合策略模型,对提高航空装备保障性评价结果的准确性和推动保障性评价技术的发展具有较大的实际应用价值。

  1. The Honorable William Nelson, Senior Senator from Florida, Chairman, Senate Committee on Space, Aeronautics and Related Sciences signing the golden book. Greeting by Mr Robert Aymar, CERN Director General and Prof. Samuel Ting from the MIT.

    CERN Multimedia

    Maximilien Brice

    2008-01-01

    The Honorable William Nelson, Senior Senator from Florida, Chairman, Senate Committee on Space, Aeronautics and Related Sciences signing the golden book. Greeting by Mr Robert Aymar, CERN Director General and Prof. Samuel Ting from the MIT.

  2. The Honorable William Nelson, Senior Senator from Florida, Chairman, Senate Committee on Space, Aeronautics and Related Sciences visiting the AMS Hall of Prevessin with Prof. Samuel Ting from the MIT.

    CERN Multimedia

    Maximilien Brice

    2008-01-01

    The Honorable William Nelson, Senior Senator from Florida, Chairman, Senate Committee on Space, Aeronautics and Related Sciences visiting the AMS Hall of Prevessin with Prof. Samuel Ting from the MIT.

  3. The Design and Implement of Aeronautical Climatic Annals%气候志分析统计的设计与实现

    Institute of Scientific and Technical Information of China (English)

    舒秦

    2015-01-01

    According to the relevant instruments for meteorology information management of CAAC, the meteorological stations, which have at least five years records of meteorological observational data for twenty-four hours or thirteen hours, should make the aeronautical climatic annals of the related civil airport. The meteorological stations should update climatic annals every years, and recognize it every five years. In this paper, a software system based on B/S systematic structure which present by compile meteoro-logical data from meteorological report system, will be used for make and analyze the aeronautical climatic annals.%按照《民用航空气象资料管理办法》,具有五年或者五年以上24小时或者13小时气象观测资料的机场气象台或者机场气象站应当编写《民用机场航空气候志》,并应逐年更新机场气候表,每五年续编一次.该文系统采用B/S架构,根据观测报表系统收集的存储观测数据,生成规定格式的气候志统计结果,用于气候志的分析与编写.

  4. 基于规则库的目视航图自动化制图%Automatic cartography for VFR aeronautical charts based on rule database

    Institute of Scientific and Technical Information of China (English)

    张文元; 许妙忠

    2011-01-01

    本文提出了一种基于规则库的目视航图自动化制图技术,详细阐述了基于规则的要素自动综合取舍、自动符号化、注记自动配置的实现方法.基于GIS COM组件开发了一个目视航图制图原型系统,通过对规则库中各种规则的配置、管理和调用,可方便快捷地制作出目视航图产品.%An automatic cartography method for VFR aeronautical charts based on rule database was introduced in this paper, and three key technologies based on rules were illustrated, including the automatization of cartographic generalization, feature symbolization and annotation placement Based on GIS Components, a prototype system of making VFR charts was developed, which could be used to make VFR aeronautical charts conveniently and quickly with the help of various pre-configured rules in rule database.

  5. Kerosene detection using laser induced fluorescence imaging for aeronautical engines application; Detection du kerozene par imagerie de fluorescence induite par laser, pour application sur foyer aeronautique

    Energy Technology Data Exchange (ETDEWEB)

    Baranger, Ph.

    2004-10-15

    The new concepts of aeronautical engines, developed to follow the evolution of the European standards of pollution, are generally based on an improvement of the processes of liquid fuel injection and mixture in the combustion chamber. There is currently no model mature enough to work without experimental validation. The purpose of this thesis is to assess the possibility of measuring the kerosene (Jet A1) vapour distribution by PLIF (Planar Laser Induced Fluorescence). That measurement technique must quantitatively image the instantaneous concentrations fields of the vaporized fuel in a spray. The implementation of such a technique needs an experimental spectroscopic study, which was realized on the vapour of fuel. First of all, this study allowed us to determine the properties of the kerosene fluorescence spectrum versus physical parameters such as temperature, pressure or gas mixture composition, especially in presence of oxygen molecules. Then, it was shown that the fluorescence spectrum of the fuel could be reproduce in all physical conditions by a single mixture of four aromatics. Their photophysical properties were also analyzed. Following this spectroscopic study, a phenomenological model for the fluorescence of the gaseous fuel was set up. This model led us to a protocol for an optical diagnostic on this fuel vapour. An experiment was set up to test the implementation and the limits of this technique in simple laboratory conditions. This experiment confirmed that this is indeed a promising technique for the diagnostic of the fuel vapour in aeronautical engine. (author)

  6. 3D mechanical analysis of aeronautical plain bearings: Validation of a finite element model from measurement of displacement fields by digital volume correlation and optical scanning tomography

    Science.gov (United States)

    Germaneau, A.; Peyruseigt, F.; Mistou, S.; Doumalin, P.; Dupré, J.-C.

    2010-06-01

    On Airbus aircraft, spherical plain bearings are used on many components; in particular to link engine to pylon or pylon to wing. Design of bearings is based on contact pressure distribution on spherical surfaces. To determine this distribution, a 3D analysis of the mechanical behaviour of aeronautical plain bearing is presented in this paper. A numerical model has been built and validated from a comparison with 3D experimental measurements of kinematic components. For that, digital volume correlation (DVC) coupled with optical scanning tomography (OST) is employed to study the mechanical response of a plain bearing model made in epoxy resin. Experimental results have been compared with the ones obtained from the simulated model. This comparison enables us to study the influence of various boundary conditions to build the FE model. Some factors have been highlighted like the fitting behaviour which can radically change contact pressure distribution. This work shows the contribution of a representative mechanical environment to study precisely mechanical response of aeronautical plain bearings.

  7. The Guggenheim Aeronautics Laboratory at Caltech and the creation of the modern rocket motor (1936-1946): How the dynamics of rocket theory became reality

    Science.gov (United States)

    Zibit, Benjamin Seth

    This thesis explores and unfolds the story of discovery in rocketry at The California Institute of Technology---specifically at Caltech's Guggenheim Aeronautics Laboratory---in the 1930s and 1940s. Caltech was home to a small group of engineering students and experimenters who, beginning in the winter of 1935--1936, formed a study and research team destined to change the face of rocket science in the United States. The group, known as the Guggenheim Aeronautics Laboratory (GALCIT, for short) Rocket Research Group, invented a new type of solid-rocket propellant, made distinct and influential discoveries in the theory of rocket combustion and design, founded the Jet Propulsion Laboratory, and incorporated the first American industrial concern devoted entirely to rocket motor production: The Aerojet Corporation. The theoretical work of team members, Frank Malina, Hsueh-shen Tsien, Homer J. Stewart, and Mark Mills, is examined in this thesis in detail. The author scrutinizes Frank Malina's doctoral thesis (both its assumptions and its mathematics), and finds that, although Malina's key assertions, his formulae, hold, his work is shown to make key assumptions about rocket dynamics which only stand the test of validity if certain approximations, rather than exact measurements, are accepted. Malina studied the important connection between motor-nozzle design and thrust; in his Ph.D. thesis, he developed mathematical statements which more precisely defined the design/thrust relation. One of Malina's colleagues on the Rocket Research Team, John Whiteside Parsons, created a new type of solid propellant in the winter of 1941--1942. This propellant, known as a composite propellant (because it simply was a relatively inert amalgam of propellant and oxidizer in non-powder form), became the forerunner of all modern solid propellants, and has become one of the seminal discoveries in the field of Twentieth Century rocketry. The latter chapters of this dissertation discuss the

  8. NASA Historical Data Book. Volume 6; NASA Space Applications, Aeronautics and Space Research and Technology, Tracking and Data Acquisition/Support Operations, Commercial Programs and

    Science.gov (United States)

    Rumerman, Judy A.

    2000-01-01

    This sixth volume of the NASA Historical Data Book is a continuation of those earlier efforts. This fundamental reference tool presents information, much of it statistical, documenting the development of several critical areas of NASA responsibility for the period between 1979 and 1988. This volume includes detailed information on the space applications effort, the development and operation of aeronautics and space research and technology programs, tracking and data acquisition/space operations, commercial programs, facilities and installations, personnel, and finances and procurement during this era. Special thanks are owed to the student research assistants who gathered and input much of the tabular material-a particularly tedious undertaking. There are numerous people at NASA associated with historical study, technical information, and the mechanics of publishing who helped in myriad ways in the preparation of this historical data book.

  9. Customer service: Re-Engineering of handling complain process the aeronautical industrial case; Re-Ingenieria en el proceso de gestion de reclamaciones. Aplicacion al sector aeronautico

    Energy Technology Data Exchange (ETDEWEB)

    Rio-Belver, R. M.; Contreras-Romeral, M. T.

    2009-07-01

    In this paper we analyze the actions carried out in Customer Care in order to improve the complaint's management system in an aeronautical company. The principles of knowledge management are taken as foundation in order to clarify the existing knowledge. A management system is designed based on knowledge of previous cases. Prior to enhance the organizations capacity and the efficiency of the process, its necessary to conduct a through re-engineering of the current process. A diagrammed turn breakdown techniques is used, brainstorming structure, the five questions, to generate the best alternatives. This big quantity of alternatives should be grouped in tasks using the affinity diagram or method Kawakita Jiro. This is achieved measurable improvements in service resolution and therefore an improvement in the products features. (Author) 7 refs.

  10. 一种航空武器数据链MAC协议设计与研究%Design and Research of Aeronautical Weapon Data Link MAC Protocol

    Institute of Scientific and Technical Information of China (English)

    段荣; 吕娜; 王翔

    2011-01-01

    MAC协议是航空武器数据链组网通信的重要技术,网络的性能依赖于所采用的多址接入协议,也是航空武器数据链研究的难点之一.固定分配、竞争和预约三大类MAC协议各有优缺点以及适应场景,需要根据应用需求设计对应的多址接入协议,以满足通信网络的战术和技术性能指标.在分析数字化战场通信网络——战术数据链组网通信应用的主要MAC协议的基础上,结合航空武器数据链的通信特点和体系结构,提出一种基于固定分配TDMA的航空武器数据链MAC协议—ODTCFMA协议,并对协议的时延性能进行了仿真和分析.分析结果表明,该协议能够同时满足编队战术协同和武器制导的低时延要求,对航空武器数据链的研究具有一定的借鉴意义.%MAC protocol is an important technology in communication network of aeronautical weapon data link, Depending on the used MAC protocol, network performance is also one of the main technical difficulties in the research of AWDL. The three kinds of MAC protocols, fixed allocation, reservation and competition, have advantages, disadvantages and adaption scene. The corresponding multiple access protocol is designed based on application requirements to meet the requirements of the tactical and technical communication network performance. The digital battlefield communications network MAC protocol is analyzed based on the combined characteristics and architecture of AWDL, and a TDM A based on fixed allocation MAC of aeronautical weapon data link;ODTCFMA protocol is proposed, then the protocol performance is simulated and analyzed. The analysis shows the MAC meets the requirements of both the for-mational tactical cooperation and the weapon guidance of low delay, which has reference significance for the research of AWDL.

  11. Virtual acoustics, aeronautics, and communications.

    Science.gov (United States)

    Begault, D R

    1998-06-01

    An optimal approach to auditory display design for commercial aircraft would utilize both spatialized (3-D) audio techniques and active noise cancellation for safer operations. Results from several aircraft simulator studies conducted at NASA Ames Research Center are reviewed, including Traffic alert and Collision Avoidance System (TCAS) warnings, spoken orientation "beacons" for gate identification and collision avoidance on the ground, and hardware for improved speech intelligibility. The implications of hearing loss among pilots is also considered.

  12. 航空产品混装PCB回流焊工艺优化%Optimizing of Mixed PCB Technology of Reflow Soldering for Aeronautical Product

    Institute of Scientific and Technical Information of China (English)

    凌月红

    2013-01-01

    SMT welding method is used more and more frequently in aeronautical electronics PCB. Many defects in spot weld such as BGA empty holes and weak jointing come from reflow soldering temperature adjustment. In this paper, the author derives the best reflow soldering temperature with oven temperature testing instruments and thrust experiments , satisfying PCB soldering quality requirements and is highly adaptable.%  目前航空电子产品印制电路板(PCB)焊接方式越来越多采用表面贴装技术(SMT),而最能体现SMT回流焊工艺能力的参数指标是回流焊曲线。很多焊点的缺陷,特别是目前较难控制与解决的球栅阵列封装器件(BGA:Ball Grid Array)空洞以及虚焊等隐性缺陷都来源于回流焊温度参数的设定。本文运用炉温测试仪和推力试验,结合实验设计获得最优化的参数设定,最终找到混装 PCB 的最佳回流炉温度曲线,满足了混装PCB焊接质量要求,且具有较强的适应能力。

  13. Dry Machining Aeronautical Aluminum Alloy AA2024-T351: Analysis of Cutting Forces, Chip Segmentation and Built-Up Edge Formation

    Directory of Open Access Journals (Sweden)

    Badis Haddag

    2016-08-01

    Full Text Available In this paper, machining aeronautical aluminum alloy AA2024-T351 in dry conditions was investigated. Cutting forces, chip segmentation, and built-up edge formation were analyzed. Machining tests revealed that the chip formation process depends on cutting conditions and tool geometry. So continuous and segmented chips are generated. Under some cutting conditions, built-up edge formation occurs. A predictive machining theory, based on a finite elements method (FEM, was applied to reproduce and explain these phenomena. Thermomechanical behaviors of the work material and the tool-work material interface were considered. Results of the proposed modelling were compared to experimental data for a wide range of cutting speed. It was shown that the feed force is well reproduced by the ALE-FE (arbitrary lagrangian-eulerian finite element formulation and highly underestimated by the lagrangian finite element (LAG-FE one. While, the periodic localized shear band, leading to a chip segmentation, is well reproduced with the Lagrangian FE formulation. It was found that the chip segmentation can be correlated to the cutting force evolution using the defined chip segmentation intensity parameter. For the built-up edge (BUE phenomenon, it was shown that it depends on the contact/friction at the tool-chip interface, and this is possible to simulate by making the friction coefficient time-dependent.

  14. Systemic culture in global manufacturing virtual networks within the aeronautical industry; Cultura sistemaca en las redes virtuales de fabricacion global de la industria aeronautica

    Energy Technology Data Exchange (ETDEWEB)

    Rodriguez-Monroy, C.

    2010-07-01

    This paper analyzes the existence of a systemic culture in global manufacturing virtual networks (GMVN). In order to validate the proposed model, based on a conceptual model of systemic culture, the case methodology have been applied to an example within the aeronautical industry that has been one of the most successful relationships within GMVNs, the collaboration between GE and SNECMA for the CFM 56 engine manufacturing. These organizations are formed by very dynamic companies that manufacture all types of products or services, and vertical relations between themselves, ( in some cases even direct competitors), where it is not necessary maintaining large internal manufacturing resources, just managing and sharing these resources efficiently in the network. This study about organizational culture at the network level includes aspects such as cultural similarity among its actors, social embeddedness, tacit knowledge transfer or the importance of trust at inter-firm collaborations. The presence under a systemic perspective, of homogeneous cultural values and practices in which network actors can be identified may strengthen the group membership or establish a social network that underlies the own GMVN and facilitates interactions among its members. The feasibility of this approach would facilitate the formation of new GMVNs, by establishing, ex ante, a cultural prescriptive model at the network level. (Author) 14 refs.

  15. Parameter Studies on High-Velocity Oxy-Fuel Spraying of CoNiCrAlY Coatings Used in the Aeronautical Industry

    Directory of Open Access Journals (Sweden)

    J. A. Cabral-Miramontes

    2014-01-01

    Full Text Available The thermal spraying process is a surface treatment which does not adversely affect the base metal on which it is performed. The coatings obtained by HVOF thermal spray are employed in aeronautics, aerospace, and power generation industries. Alloys and coatings designed to resist oxidizing environments at high temperatures should be able to develop a surface oxide layer, which is thermodynamically stable, slowly growing, and adherent. MCrAlY type (M = Co, Ni or combination of both coatings are used in wear and corrosion applications but also provide protection against high temperature oxidation and corrosion attack in molten salts. In this investigation, CoNiCrAlY coatings were produced employing a HVOF DJH 2700 gun. The work presented here focuses on the influences of process parameters of a gas-drive HVOF system on the microstructure, adherence, wear, and oxygen content of CoNiCrAlY. The results showed that spray distance significantly affects the properties of CoNiCrAlY coatings.

  16. Automotive and aeronautical clusters in the São Paulo state’s Vale do Paraíba: a comparison of formation trajectories

    Directory of Open Access Journals (Sweden)

    Márcio da Silveira Luz

    2010-04-01

    Full Text Available This paper presents a comparison of the relevant characteristics of São Paulo State’s Vale do Paraíba automotive and aerospace clusters observed and analyzes the technological and productive chains strengthening. In order to accomplish it, the adopted methodological procedures are of qualitative nature, by means of documentary research. The results pointed out that the government established, in the mid-1945, the currently named Departamento de Ciência e Tecnologia Aeroespacial (DCTA, as a research and development (R&D center and, by 1979, Embraer, a state-owned aeronautical construction industry. It was also sought to generate conditions so that domestic companies could emerge around and replace the dependency on aerospace systems and subsystems international suppliers by developing indigenous technological capacities. The automotive cluster under study started in the São Paulo State’s Vale do Paraíba (PPV by means of the regionalization of multinational automotive construction firms migrated from ABC Paulista region looking for physical space for their growth, also relying on tax benefits. The survey results indicate that, in spite of fundamental differences with regard to their productive chains strenghtening processes, they showed similar adverse results.

  17. 航务报文处理系统的分析与设计%Analysis and Design of Aeronautical Telex Processing System

    Institute of Scientific and Technical Information of China (English)

    何国斌; 马世龙

    2001-01-01

    航务报文处理系统是对民航系统中充当部门间信息交换媒介的航务报文进行处理的软件系统,可以在民航多个部门中得到广泛应用.当前已有的航务报文处理系统存在通用性不好、可集成性差以及信息发布方式不合理等缺点.ATPS(Aeronautical Telex Processing System) 2.0航务报文处理系统就是针对这些问题,在对航务报文处理业务以及已有系统进行分析的基础上,综合使用UML(Unified Modeling Language)、中间件以及构件等多种技术的航务报文处理系统.

  18. Child health promotion program in South Korea in collaboration with US National Aeronautics and Space Administration: Improvement in dietary and nutrition knowledge of young children

    Science.gov (United States)

    Lim, Hyunjung; Kim, JiEun; Min, Jungwon; Carvajal, Nubia A.; Lloyd, Charles W.

    2016-01-01

    BACKGROUND/OBJECTIVES Childhood obesity has become a global epidemic. Development of effective and sustainable programs to promote healthy behaviors from a young age is important. This study developed and tested an intervention program designed to promote healthy eating and physical activity among young children in South Korea by adaptation of the US National Aeronautics and Space Administration (NASA) Mission X (MX) Program. SUBJECTS/METHODS The intervention program consisted of 4 weeks of fitness and 2 weeks of nutrition education. A sample of 104 subjects completed pre- and post-surveys on the Children's Nutrition Acknowledgement Test (NAT). Parents were asked for their children's characteristics and two 24-hour dietary records, the Nutrition Quotient (NQ) at baseline and a 6-week follow-up. Child weight status was assessed using Korean body mass index (BMI) percentiles. RESULTS At baseline, 16.4% (boy: 15.4%; girl: 19.2%) of subjects were overweight or obese (based on BMI≥85%tile). Fat consumption significantly decreased in normal BMI children (48.6 ± 16.8 g at baseline to 41.9 ± 18.1 g after intervention, P NASA MX project is feasible and shows favorable changes in eating behaviors and nutritional knowledge among young children. PMID:27698964

  19. Maintenance Support Ability Evaluation Model of Aeronautical Equipment Based on Weighted LS-SVM%加权LS-SVM的航空装备维修保障能力评估模型

    Institute of Scientific and Technical Information of China (English)

    胡新江; 徐浩军; 王文栋; 揭军魂

    2012-01-01

    Maintenance support ability evaluation work is an important content of aeronautical equipment whole-system and whole-life management. The scientific and precise evaluation method of maintenance support ability is the base to achieve the precise support of aeronautical equipment. Firstly, the evaluation guideline system of aeronautical equipment maintenance support ability is established. Then the key factor guidelines are made sure. Finally, the evaluation model of aeronautical equipment maintenance support ability based on Weighted LS-SVM is established. The simulation results show that the method is valid.%维修保障能力评估工作是航空装备全系统全寿命管理的一项重要内容,科学精确的维修保障能力评估方法是实现航空装备精确化保障的基础.首先建立了航空装备维修保障能力评估指标体系,确定了关键要素指标,然后建立了基于加权LS-SVM的航空装备维修保障能力评估模型,仿真结果验证了该方法的有效性.

  20. Computer Aided Optimization Design of Riveted Joints in Aeronautics%计算机辅助飞机铆钉连接优化设计

    Institute of Scientific and Technical Information of China (English)

    高原; 于随然

    2014-01-01

    飞机铆钉连接设计涉及设计部门与计算部门,部门之间的数据交流过程不仅浪费大量时间,而且也会因为配合不协调导致数据版本等出现错误。为了优化飞机铆钉连接设计流程,文章提出了一种结合两个部门功能并利用设计者自身知识的计算机辅助设计方法,其核心是一个能够从多方面综合评价铆钉连接设计的算法以及一个友善的用户界面。将方法应用于SaM146涡轮发动机机舱铆钉连接设计,验证了其有效性。%Riveted joints design includes the design department and the calculation department. During the transmission of information between the two departments, a lot of time is wasted and it can easily lead to desynchroni-zation between departments. To optimize the design process of riveted joints in aeronautics, a method was brought out to solve this problem by combining the functions of these two departments and, at the same time, taking advantage of the designers’ expertise. The key elements of this method were a friendly user interface and an algorithm which can e-valuate riveted joints design from several aspects. Finally this method is applied to a riveted joints design in the na-celle of SaM146 turbofan engine and thus proves this method is both effective and efficient.

  1. Characterization of Ni19.5Ti50.5Pd25Pt5 High-Temperature Shape Memory Alloy Springs and their Potential Application in Aeronautics

    Science.gov (United States)

    Stebner, Aaron; Padula, Santo A.; Noebe, Ronald D.

    2008-01-01

    Shape memory alloys (SMAs) have been used as actuators in many different industries since the discovery of the shape memory effect, but the use of SMAs as actuation devices in aeronautics has been limited due to the temperature constraints of commercially available materials. Consequently, work is being done at NASA's Glenn Research Center to develop new SMAs capable of being used in high temperature environments. One of the more promising high-temperature shape memory alloys (HTSMAs) is Ni19.5Ti50.5Pd25Pt5. Recent work has shown that this material is capable of being used in operating environments of up to 250 C. This material has been shown to have very useful actuation capabilities, demonstrating repeatable strain recoveries up to 2.5% in the presence of an externally applied load. Based on these findings, further work has been initiated to explore potential applications and alternative forms of this alloy, such as springs. Thus, characterization of Ni19.5Ti50.5Pd25Pt5 springs, including their mechanical response and how variations in this response correlate to changes in geometric parameters, are discussed. The effects of loading history, or training, on spring behavior were also investigated. A comparison of the springs with wire actuators is made and the benefits of using one actuator form as opposed to the other discussed. These findings are used to discuss design considerations for a surge-control mechanism that could be used in the centrifugal compressor of a T-700 helicopter engine.

  2. 新概念下航空产品科研生产流程探讨%Discussion on Scientific Research and Production Flow of Aeronautical Products Under New Concept

    Institute of Scientific and Technical Information of China (English)

    吴志恩

    2001-01-01

    Rapid development of scientific technology, especially information technology brings to scientific research and production of the aeronautical products a series of new changes. In this paper, a new thinking in establishing scientific research and production of aeronautical products flow are discussed based on the conditions in China. At the same time, the agile manufacture and lean production are described in detail.%随着现代科学技术尤其是信息技术的快速发展,航空产品的科研生产出现了一系列新的变化。本文结合我国国情,探讨了制定航空产品科研生产流程的新思路,并对敏捷制造和精益生产作了较详细的叙述

  3. The development of turbojet aircraft in Germany, Britain, and the United States: A multi-national comparison of aeronautical engineering, 1935--1946

    Science.gov (United States)

    Pavelec, Sterling Michael

    In the 1930s aeronautical engineering needed revision. A presumptive anomaly was envisaged as piston-engine aircraft flew higher and faster. Radical alternatives to piston engines were considered in the unending quest for speed. Concurrently, but unwittingly, two turbojet engine programs were undertaken in Europe. The air-breathing three-stage turbojet engine was based on previous turbine technology; the revolutionary idea was the gas turbine as a prime mover for aircraft. In Germany, Dr. Hans von Ohain was the first to complete a flight-worthy turbojet engine for aircraft. Installed in a Heinkel designed aircraft, the Germans began the jet age on 27 August 1939. The Germans led throughout the war and were the first to produce jet aircraft for combat operations. The principal limiting factor for the German jet program was a lack of reliable engines. The continuing myths that Hitler orders, too little fuel, or too few pilots hindered the program are false. In England, Frank Whittle, without substantial support, but with dogged determination, also developed a turbojet engine. The British came second in the jet race when the Whittle engine powered the Gloster Pioneer on 15 May 1941. The Whittle-Gloster relationship continued and produced the only Allied combat jet aircraft during the war, the Meteor, which was confined to Home Defense in Britain. The American turbojet program was built directly from the Whittle engine. General Electric copied the Whittle designs and Bell Aircraft was contracted to build the first American jet plane. The Americans began the jet age on 1 October 1942 with a lackluster performance from their first jet, the Airacomet. But the Americans forged ahead, and had numerous engine and airframe programs in development by the end of the war. But, the Germans did it right and did it first. Partly because of a predisposition towards excellent engineering and physics, partly out of necessity, the Germans were able to produce combat turbojet aircraft

  4. Research on Improving Teachers' Professional Quality of Higher Vocational Aeronautic Maintenance Major%提高高职航空维修类教师的职业素养的研究

    Institute of Scientific and Technical Information of China (English)

    谭卫娟

    2012-01-01

    The key to vigorously develop vocational education is to build a high-quality teacher team. Aeronautic maintenance major closely centers development of military aviation and civil aviation, setting up this major is to serve regional economic development, and it belongs to "industrial support". Whether can train high-end skilled personnel of aeronautic maintenance major who are able to work in less well conditions, be employed and remained and create performance lies in the way of improving professionalism of the teachers of aeronautic maintenance major.%大力发展职业教育,关键在于建设一支高质量的教师队伍.航空维修类专业,是紧紧围绕我国军用航空与民用航空发展,服务区域经济发展开办的专业,属于“产业支撑型”专业.是否能培养出“下得去、用得上、留得住、出业绩”的航空维修类高端技能型人才,前提在于如何提高航空维修类教师的职业素养.

  5. SWOT analysis of Beijing institute of aeronautical materials’ polymer matrix composites professional%北京航空材料研究院树脂基复合材料专业SWOT分析

    Institute of Scientific and Technical Information of China (English)

    刘旸; 孙沛; 何鲁林

    2012-01-01

    The advantages,disadvantages,opportunities and threats during the process of development of Beijing institute of aeronautical materials composites were reviewed in this paper.The future development was also discussed: the next great development in composite materials would be an asset and a challenge for Beijing institute of aeronautical materials.If Beijing institute of aeronautical materials could give full play to their technology advantages,and resolve appropriately the problem,the great success will be wined in the future.%综述北京航空材料研究院复合材料专业的优、劣势和面临发展的机遇和威胁,并就未来发展提出了一些观点。指出复合材料的大发展既是对北京航空材料研究院的挑战,同样也是机遇,北京航空材料研究院在充分发挥自身技术优势的同时,正视并解决存在的劣势和不足,主动把握发展机遇,必将在未来取得更大的成功。

  6. 基于量子遗传算法的航空通信频率动态分配%Dynamic Aeronautical Communication Frequency Assignment Based on Quantum Genetic Algorithm

    Institute of Scientific and Technical Information of China (English)

    徐雪飞; 李建华; 沈迪; 郭蓉

    2015-01-01

    For more efficient aeronautical communication frequency assignment,a method for dynamic aero-nautical communication frequency assignment based on quantum genetic algorithm ( QGA ) is proposed. Through analyzing the thought of dynamic frequency assignment,the architecture of dynamic frequency as-signment is constructed,then a flow chart for it is given. On this basis,the dynamic aeronautical communi-cation frequency assignment problems are discussed,the constraint condition for dynamic frequency assign-ment is defined,and then the dynamic aeronautical communication frequency assignment model is estab-lished. Finally, the QGA and genetic algorithm( GA) are used to simulate the same examples and the re-sult shows that the QGA has more advantages in population fitness and convergence rate,and the dynamic frequency assignment model can dynamically adjust fitness under the condition of different populations. The method meets the practice and application requirements of dynamics,accuracy and timeliness for aero-nautical communication frequency assignment.%为了更加有效地对航空通信频率进行分配,提出了一种基于量子遗传算法的航空通信频率动态分配方法。通过对频率动态分配思路进行分析,建立了频率动态分配框架,给出了频率动态分配的具体流程。在此基础上,讨论了航空通信频率动态分配问题,定义了航空通信频率动态分配约束条件,建立了航空通信频率动态分配模型。最后,运用量子遗传算法和遗传算法对算例进行仿真对比。结果表明:量子遗传算法在种群适应度和收敛速度上具备明显的优越性,频率动态分配模型能够根据不同种群数量条件动态调整适应度,能够较好满足航空通信频率分配问题动态性、准确性、时效性等实践运用要求。

  7. Estabelecimento de ciclo de cura de pré-impregnados aeronáuticos Establishment of cure cycle of aeronautic prepregs

    Directory of Open Access Journals (Sweden)

    Michelle L. Costa

    2005-07-01

    Full Text Available Os compósitos poliméricos podem ser produzidos via moldagem em autoclave, onde as condições de processamento podem ser otimizadas a partir do conhecimento físico-químico da matriz polimérica. A evolução da cinética da reação de cura ocorre simultaneamente com as modificações no comportamento reológico do sistema polimérico, sendo comum denominar o fenômeno de comportamento reo-cinético. O presente trabalho tem como objetivo conhecer os parâmetros de cura, cinéticos e reológicos, de três diferentes sistemas de pré-impregnados de resina epóxi (cura a 177 °C, conhecidos como F161, F584 e 8552, hoje usados na indústria aeronáutica brasileira. Este estudo foi realizado com o auxílio das técnicas de DSC e reologia, utilizando-se análises dinâmicas e isotérmicas. Com isso, foi possível estabelecer a ordem de reação e a cinética de cura dos sistemas estudados. Neste estudo, foram utilizados como modelos matemáticos o de ordem n e o autocatalítico com ordem total de aproximadamente 2. A temperatura de gel foi de ~100 °C, e o tempo de gel correspondente foi de 135 segundos. A partir do conhecimento da cinética de cura e dos parâmetros reológicos dos sistemas de pré-impregnados foi possível estabelecer um ciclo de cura destinado à consolidação das peças aeronáuticas via moldagem em autoclave.Autoclave molding produces polymer composites, where the processing conditions can be optimized with physicochemical knowledge of the polymeric matrix. The cure reaction evolves simultaneously with changes in rheology, which is normally refered to as rheo-kinetic behavior. With the knowledge of the appropriate cure cycle one can identify the steps in which pressure should be applied and when to raise the temperature. This paper is aimed at investigating the cure, kinetics and rheological parameters of three prepreg epoxy systems, namely F161, F584 and 8552, which are currently used in the Brazilian aeronautic industry

  8. High-temperature polyimide composites and its application in aeronautical engine%航空发动机用PMR聚酰亚胺树脂基复合材料

    Institute of Scientific and Technical Information of China (English)

    谭必恩; 益小苏

    2001-01-01

    This paper reviewed the progress of high-temperature PMR type polyimide matrix composites, and summarized its application in aeronautical engine field.%较全面地综述了PMR聚酰亚胺树脂及其复合材料的制备、性能,并总结了其在航空发动机上的应用情况,分析了目前存在的问题,并提出了将来可能的发展方向。

  9. 高分辨率可见光航空相机的热设计及热分析%Thermal design and analysis for the high resolution visible light aeronautic camera

    Institute of Scientific and Technical Information of China (English)

    王领华; 吴清文; 郭亮; 刘伟毅; 陈立恒

    2012-01-01

    In order to ensure the aeronautic camera working in the complex environment could fulfill its task successfully, the thermal design was presented. The corresponding thermal environment was established and the calculating method of the environmental heat fluxes and heat-transfer model of the camera was provided. The environment of the aeronautic camera was analyzed, and its requirements of thermal control was stated. The thermal control pattern of the aeronautic camera was depicted. In addition,the finite element model was built and the camera's two extreme conditions was simulated with the IDEAS-TMG software. In the extreme conditions, the results of the simulation indicate that: the temperature level of the primary mirror tube is 18±1℃; the axial temperature of the primary mirror tube is no more than 1.5 t; the circle temperature of the primary mirror tube is no more than 1.85℃, which could satisfy the requirements. The results of the simulation indicate that the thermal design is feasible and reasonable. The research jobs could give some guidance and reference for other aeronautic camera.%为了确保工作在复杂环境中的航空相机能顺利完成任务,对其热控制技术进行了研究.分析了相机的热环境,建立了其换热模型并给出了外热流的计算方法.针对航空相机所处的复杂飞行环境及所需的热控指标,详细阐述了相机的热设计方案,利用热分析软件IDEAS-TMG建立了相机的有限元模型并对相机的两个极端工况进行了仿真分析.仿真分析结果表明:在两个极端工况中,主镜筒温度水平18±1℃、主镜筒轴向温差不大于1.5℃和周向温差不大于1.85℃,均达到了热控指标要求,热设计方案合理可行.该研究方法对各类航空相机的热设计和热分析有一定的指导和借鉴作用.

  10. Filmes de nanodiamantes para aplicações em sistemas eletroquímicos e tecnologia aeroespacial Nanodiamond films for applications in electrochemical systems and aeronautics and space technology

    Directory of Open Access Journals (Sweden)

    Adriana Faria Azevedo

    2006-02-01

    Full Text Available The goal of this work is to show the use of undoped nanodiamond films as a new material for electrochemical and aerospace applications. Correlation between the applications and physico-chemical features of nano and conventional CVD polycrystalline diamond films are presented. An important and innovative application of these nanodiamonds is organic electrosynthesis, including pharmaceutical and water disinfection products, as well as electroanalytical applications, for example, development of biosensors for detection of glucose, glutamate and dopamine. In aeronautics and space developments, these nanodiamonds could be used as electrodes in rechargable batteries and in tribological investigations.

  11. 航空高职学院毕业生就业见习实习基地建设研究%On Aeronautical Vocational College Graduates' Job Attachment Practice Base

    Institute of Scientific and Technical Information of China (English)

    胡良君; 王红梅; 宋锐; 李晓锋

    2013-01-01

      “航空高职学院毕业生就业见习实习基地”旨在解决航空职院毕业生缺乏工作经验,增加毕业生就业见习实习实践的机会,有效提高毕业生的就业率。%The aeronautical vocational college graduates' job attachment practice base aims to address solve the problem of aviation Vocational-Technical College graduates' lack of work experience, increase graduates' opportunity to practice, and effectively improve the employment rate of graduates.

  12. Discussion on the Material Chemistry Course Construction for the University of Aeronautics and Astronautics%航空航天院校材料化学课程建设探讨

    Institute of Scientific and Technical Information of China (English)

    姬广斌

    2011-01-01

    本文从材料化学在航空航天领域所处的地位讲起,作者结合在材料化学课程讲授中的体会,在教材建设、教学内容、教学方法、教学手段、考核方式和实验教学等方面进行了有益的探索和实践。%According to the position of material chemistry in the field of aeronautics and astronautics,and based on the author's experience in Material Chemistry Course teaching,some valuable exploration and practice on textbook construction,course contents,teachin

  13. Digital, Satellite-Based Aeronautical Communication

    Science.gov (United States)

    Davarian, F.

    1989-01-01

    Satellite system relays communication between aircraft and stations on ground. System offers better coverage with direct communication between air and ground, costs less and makes possible new communication services. Carries both voice and data. Because many data exchanged between aircraft and ground contain safety-related information, probability of bit errors essential.

  14. Unsteady computational fluid dynamics in aeronautics

    CERN Document Server

    Tucker, P G

    2014-01-01

    The field of Large Eddy Simulation (LES) and hybrids is a vibrant research area. This book runs through all the potential unsteady modelling fidelity ranges, from low-order to LES. The latter is probably the highest fidelity for practical aerospace systems modelling. Cutting edge new frontiers are defined.  One example of a pressing environmental concern is noise. For the accurate prediction of this, unsteady modelling is needed. Hence computational aeroacoustics is explored. It is also emerging that there is a critical need for coupled simulations. Hence, this area is also considered and the tensions of utilizing such simulations with the already expensive LES.  This work has relevance to the general field of CFD and LES and to a wide variety of non-aerospace aerodynamic systems (e.g. cars, submarines, ships, electronics, buildings). Topics treated include unsteady flow techniques; LES and hybrids; general numerical methods; computational aeroacoustics; computational aeroelasticity; coupled simulations and...

  15. 14 CFR 61.109 - Aeronautical experience.

    Science.gov (United States)

    2010-01-01

    ... tower. (j) For a weight-shift-control aircraft rating. A person who applies for a private pilot...-country flight training in a weight-shift-control aircraft; (2) Except as provided in § 61.110, 3 hours of night flight training in a weight-shift-control aircraft that includes— (i) One cross-country...

  16. Aeronautic Instruments. Section IV : Direction Instruments

    Science.gov (United States)

    Franklin, W S; Stillman, M H; Sanford, R L; Warner, John A C; Sylvander, R C; Rounds, E W

    1923-01-01

    Part one points out the adequacy of a consideration of the steady state gyroscopic motion as a basis for the discussion of displacements of the gyroscope mounted on an airplane, and develops a simple theory on this basis. Principal types of gyroscopic inclinometers are described and requirements stated. Part two describes a new type of stabilizing gyro mounted on top of a spindle by means of a universal joint, the spindle being kept in a vertical position by supporting it as a pendulum of which the bob is the driving motor. Methods of tests and the difficulties in designing a satisfactory and reliable compass for aircraft use in considered in part three. Part four contains a brief general treatment of the important features of construction of aircraft compasses and description of the principal types used.

  17. Aeronautical Decision Making for Helicopter Pilots

    Science.gov (United States)

    1987-02-01

    on the original goal or destination combined with a total disregard for any alternative courses of action. Duck-Under Sindrome - The tendency to "sneak...fellow down . 48 Response to Situation Al: Alternative a; By acting in a superior way, you are being macho, thinking, ŕ can do it." Go back to Situation...you have flown through light clouds before in daylight. d. You figure that you can always Set air traffic control to talk you down . e. You just want

  18. Optimal Nuclear Radiation Criteria for Aeronautical Systems

    Science.gov (United States)

    1981-05-15

    decrease in needed keep out rang would reduce the Vi required bean- pomer-on- tarot by a factor of 3, (or tore, if scattering, beam dispersal and other...to continuing, a brief discussion of the type of responses/effects caused by each of the environments should aid the reader . The neutrons cause

  19. Chart Supplements - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — The Chart Supplements are searchable by individual airport in PDF format. They contain data on public and joint use airports, seaplane bases, heliports, VFR airport...

  20. Equalization in Aeronautical Telemetry Using Multiple Antennas

    Science.gov (United States)

    2014-04-01

    SOQPSK-TG) and a version of non-binary, multi-index continuous phase modulation ( CPM ) called ARTM CPM . PCM/FM is the legacy modulation which, relative...TG is a continuous phase modulation ( CPM ) whose complex-valued baseband equivalent represen- tation [12] is x(t,α) = √ 2Eb Tb exp [j (φ(t,α) + φ0...TG is a partial response CPM . Consequently, the maximum likeli- hood detector in the additive white Gaussian noise (AWGN) environment is a sequence

  1. Transonic aeroelastic numerical simulation in aeronautical engineering

    Energy Technology Data Exchange (ETDEWEB)

    Yang, G. [Chinese Academy of Sciences, LHD of the Inst. of Mechanics, Beijing (China)]. E-mail: gwyang@imech.ac.cn

    2005-07-01

    An LU-SGS (lower-upper symmetric Gauss-Seidel) subiteration scheme is constructed for time-marching of the fluid equations. The HLLEW (Harten-Lax-van Leer-Einfeldt-Wada) scheme is used for the spatial discretization. The same subiteration formulation is applied directly to the structural equations of motion in generalized coordinates. Through subiteration between the fluid and structural equations, a fully implicit aeroelastic solver is obtained for the numerical simulation of fluid/structure interaction. To improve the ability for application to complex configurations, a multiblock grid is used for the flow field calculation and Transfinite Interpolation (TFI) is employed for the adaptive moving grid deformation. The infinite plate spline (IPS) and the principal of virtual work are utilized for the data transformation between the fluid and structure. The developed code was first validated through the comparison of experimental and computational results for the AGARD 445.6 standard aeroelastic wing. Then the flutter character of a tail wing with control surface was analyzed. Finally, flutter boundaries of a complex aircraft configuration were predicted. (author)

  2. Aeronautical Decision Making - Cockpit Resource Management

    Science.gov (United States)

    1989-01-01

    drinking is the primary coping response to stress, obesity or alcoholism is like to present its own problems. It is a bad idea to use ’addictive...proper foods to keep me adequately nourished during the entire flight? 64 REFERENCES Aufderheide, E.H. Aircrew Gordination Training: A Military Airlift...statement to the Board included the following: "I commented to my crew, ’look at the junk on that airplane’,.. .Almost the entire length of ý_’Lie

  3. 14 CFR 61.129 - Aeronautical experience.

    Science.gov (United States)

    2010-01-01

    ... 2-hour cross country flight in a multiengine airplane in daytime conditions that consists of a total...-hour cross country flight in a multiengine airplane in nighttime conditions that consists of a total... point of departure; and (iii) One hour cross country flight in an airship in nighttime conditions...

  4. Fundamentals of Aeronautical and Aerospace Medical Science,

    Science.gov (United States)

    1981-07-17

    spleen , duodenum. . Metabolism of water and salt: As for the physiological responses to anoxia, the symptom of respiratory alkali toxication...especially the liver, spleen and digestive tract. A large quantity of blood will then floq frm the internal organs toward the skin and muscle, bringing...emergency treatment is to move the patient to a shady place, loosen the clothes, and place ammonia under patient’s nose to wake up the patient. The general

  5. Air Force Academy Aeronautics Digest - Fall 1979.

    Science.gov (United States)

    1980-04-01

    around it. This geocentric system was first advanced by the Greeks, refined by Cladius Ptolemy (A.D. 200) and adopted as truth by the Church in Western...Europe (Ref. 2). This earth-centered system was staunchly supported until the sixteenth century when Nicolaus Copernicus began to develop a different...line of thought. Copernicus believed that the earth and other planets revolved around the sun in a heliocentric system and published his hypothesis in

  6. System Design for FEC in Aeronautical Telemetry

    Science.gov (United States)

    2012-03-12

    ORGANIZATION REPORT NUMBER AFFTC-PA-12070 9. SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES) Tom Young , EA Air Force Flight Test Center...uG = [u uW ], where the arithmetic is performed modulo -2. When transmitting an LDPC code word, the SOQPSK modulator is operated without...The arithmetic is performed modulo -2. The encoder has one output stream containing the information bits (without alteration) and one output stream

  7. Multilingual Aeronautical Dictionary (Dictionnaire Aeronautique Multilingue)

    Science.gov (United States)

    1980-01-01

    ES resistencia ff) doe cantidlad do moto del atre 10327 P0 indicador Wm do posipolar (API) FIR zraiirae 0)I due i Ia quantitii do modvement air...Azimutalkreis (in TU tUm kuyruk kontrollu upak NE legering 3 Hbhenparallelkreis (m) 136P0 liga 0)I ES almicantarat Wm136RU cnnao Wm FR 1. almicantarat...leghe (f, pl di alluminio 10456 abiCOTHeiX ycnosnl NE alummiumlegeringen (pl) American Ephemeris An annual pubicatin TU irtifa deney tezghi PO ligas

  8. Aeronautical Wind Tunnels, Europe and Asia

    Science.gov (United States)

    2006-02-01

    closed-circuit wind tunnel, 8-kW motor. Operates at sub-freezing temperatures. Built of wood and epoxy-fiberglass composite. Internally insulated with...airplane models. Also used to test wind loads on buildings, bridges, radar antennas, and television towers, and aerodynamic performance of windmills ...flow. This facility has a mahogany six- bladed fan powered by a 2000-hp, 750-V DC motor. At full speed this facility can run at 1.5 MVA. Data

  9. Aeronautical Engineering. A Continuing Bibliography with Indexes

    Science.gov (United States)

    1987-09-01

    basis and a means FAHREN FUER REIBUNGSFREIE UND REIBUNGSBEHAFTETE of numerical simulation for further improving the design of turbine...tegrated with additional on-board sensors to yield a complete danger-warning systems and radio navigation and landing id autonomous navigation system. O.C...Examples of the use of such systems are described, including their application as autonomous assistants in cockpits and as man/machine interfaces in flight

  10. Research on the Course Reform of Electrical Power Supply System of Aeronautics and Astronautics%“航空航天供电系统”的课程改革研究

    Institute of Scientific and Technical Information of China (English)

    杨善水; 王莉; 张卓然

    2012-01-01

    航空航天供电系统是航空类电气工程与自动化本科专业的特色专业课程。航空供电系统包括发电、电能变换和配电等多个重要环节,该课程最突出特点是系统性强。在实际的教学中,应从系统基本功能需求分析和可靠性要求等方面突出系统性的概念,而不局限于部件的性能分析;应联系实际科研情况,阐明未来的发展方向。%Electrical Power Supply System of Aeronautics and Astronautics is a special course for the students majo- ring in electrical engineering and automation specialty. The electrical power supply system is composed by some parts such as power generation, converting, and distribution, etc. In the course, the systematization of system should be emphasized from some aspects such as the fundamental function requirements, reliability requirements, rather than be restricted in the analysis of some parts of the system. The research work of the teacher and the develop- ment of the electrical power supply system should be integrated into the education

  11. Development of a 3-D model for eddy current testing: application for fastened structures in aeronautics; Developpement d'un modele pour le controle non destructif par courants de Foucault de structures rivetees en aeronautique

    Energy Technology Data Exchange (ETDEWEB)

    Paillard, S

    2007-12-15

    One of the Eddy Current Testing issues in aeronautics is the inspection of fastened structures to detect flaws nearby rivets which can grow because of mechanical stress. EADS and the CEA LIST have started a collaborative work with the support of the Ile-de-France Region to develop a simulation tool of EC fastened structures testing, integrated to the CIVA platform, aimed at conceiving testing methods, optimizing and qualifying it. The volume integral method using the Green dyadics formalism has been chosen in order to get a fast resolution of Maxwell equations. A first milestone was to build a simulation model of multilayer structures testing, thanks to the use of the multilayer Green dyads. Because of the rivet volume, 60 times bigger than the one of a typical flaw, a large number of discretization cells are needed. Therefore an iterative method has been developed in order to numerically solve large calculation zones. Finally, the flaw response simulation mostly has to cope with a scale issue between the size of the rivet and the one of the flaw, the latter being much smaller in a direction than the former. The whole model has been experimentally validated and compared to other simulation models at the important development steps: multilayer configuration, iteration resolution, and flaw signature. (author)

  12. Senior Senator from Florida and Chairman, Senate Committee on Space, Aeronautics and Related Sciences W. Nelson, visiting the ATLAS cavern and LHC tunnel with ATLAS Collaboration Spokesperson P. Jenni and AMS Collaboration Spokesperson S.C.C.Ting, 16 March 2008.

    CERN Multimedia

    Maximilien Brice

    2008-01-01

    Senior Senator from Florida and Chairman, Senate Committee on Space, Aeronautics and Related Sciences W. Nelson, visiting the ATLAS cavern and LHC tunnel with ATLAS Collaboration Spokesperson P. Jenni and AMS Collaboration Spokesperson S.C.C.Ting, 16 March 2008.

  13. “航空电机及电气传动”课程机辅教学实践%Teaching Practice of Aeronautical Motor and Electrical Drive Course

    Institute of Scientific and Technical Information of China (English)

    高洁; 高冰; 刘建英; 郝魁红

    2014-01-01

    本文以“航空电机及电气传动”课程中开关磁阻电机及其系统为例,利用电磁场有限元分析及电力电子仿真软件,以电机的基本结构、工作原理、工作特性和应用场合为主线,进一步直观呈现其磁场分布及电气传动系统运行曲线,使得理论教学内容紧密结合工程实际。本文所述的软件对于其他电机及其电气传动系统的教学具有一定的参考价值,亦可用于学生本科毕业设计环节。%This paper takes switched reluctance motor and system in Aeronautical Motor and Electric Drire course for example,using finite element analysis and power electronics simulation software,and with the main line of basic structure,work principle and properties application,showing the magnetic field distribution and operation curve of electric motor drive system. So that the theoretical study can be closely integrated with practice. Software described in this paper has some reference value for the teaching of other special motors and electrical drive systems,and also can be used in graduate design.

  14. 适于航空高压直流供电的1kW LLC全桥变换器%A 1 kW LLC Full-bridge Converter for Aeronautic High Voltage DC Power Supply

    Institute of Scientific and Technical Information of China (English)

    张超; 管松敏; 陈乾宏

    2011-01-01

    With the development of the electric technology, aircraft is developing forward the goal of more electric aircraft. As the 270 V high voltage DC power supply system has many advantages such as reliable,light weight and high effficiency,it has become the trend of the power supply system in aircraft. In the application of the aeronautic DC/DC conversion,the LLC full-bridge resonant converter is a kind of ideal topologies. When constructing the resonant inductor with the leakage inductance of the transformer, the secondary leakage inductance must be converted to the primary equally. However there is no such paper discussing about this in detail. Experimental results are presented by a prototype with its input (270±10%) V output 28.5 V/1 kW.The turn ratio difference between the two transformer models can be verified successfully by the experimental results.%随着电气技术水平的提高,飞机正向"多电飞机"的目标发展.270 V高压直流电源系统具有安全可靠、重量轻及节省电能等优点,成为现阶段飞机供电系统的发展方向.在航空中大功率DC/DC变换的应用场合,LLC全桥谐振变换器是一种较理想的拓扑.利用变压器漏感构造谐振电感时,必须将次级漏感等效至初级,而目前很少有文献对其进行分析设计.经研究发现,等效后的匝比相对物理匝比偏小.制作了一台输入直流电压为(270±10%)V,输出为28.5 V/1 kW的原理样机,且对根据物理匝比、等效匝比计算得到的理论增益特性与实验测得的增益特性进行了比较分析,说明了变压器等效模型的正确性.

  15. Corrosión de Aleaciones Aeronáuticas de Aluminio y sus Componentes Relacionada a la Expresión Proteica del Hongo Hormoconis resinae Corrosion of Aeronautical Aluminium Alloys and its Components Related to the Proteic Expression of the Fungus Hormoconis resinae

    Directory of Open Access Journals (Sweden)

    Raquel Araya

    2008-01-01

    Full Text Available Este artículo muestra que los requerimientos nutricionales de oligoelementos constituyen la fuerza impulsora de la corrosión influenciada microbiológicamente que produce Hormoconis resinae en aleaciones aeronáuticas de aluminio. Se compararon perfiles proteicos de biopelículas del hongo cultivado en turbocombustible aeronáutico mediante electroforesis en geles de poliacrilamida. Se caracterizó la morfología de ataque de las aleaciones y de sus componentes metálicos puros y el crecimiento de hifas sobre cada metal mediante microscopía electrónica de barrido ambiental. Se concluyó que la corrosión estaría asociada a aleantes que actuarían como oligoelementos para el microorganismo.This article shows that the metabolic needs of oligoelements constitute the driving force of the microbiologically influenced corrosion produced by Hormoconis resinae on aeronautical aluminium alloys. Protein profiles of biofilms generated by fungal strains cultivated in aeronautical fuel were compared by electrophoresis in poliacrylamide gels. The morphology attack of alloys, its component metals and the growth of hyphae in cultures were characterized by means of environmental scanning electronic microscopy. One of the main conclusions is that corrosion would be associated to alloying elements that would act as oligoelements for the microorganism.

  16. Turbulent combustion modelization via a tabulation method of detailed kinetic chemistry coupled to Probability Density Function. Application to aeronautical engines; Modelisation de la combustion turbulente via une methode tabulation de la cinetique chimique detaillee couplee a des fonctions densites de probabilite. Application aux foyers aeronautiques

    Energy Technology Data Exchange (ETDEWEB)

    Rullaud, M.

    2004-06-01

    A new modelization of turbulent combustion is proposed with detailed chemistry and probability density functions (PDFs). The objective is to capture temperature and species concentrations, mainly the CO. The PCM-FTC model, Presumed Conditional Moment - Flame Tabulated Chemistry, is based on the tabulation of laminar premixed and diffusion flames to capture partial pre-mixing present in aeronautical engines. The presumed PDFs is introduced to predict averaged values. The tabulation method is based on the analysis of the chemical structure of laminar premixed and diffusion flames. Hypothesis are presented, tested and validated with Sandia experimental data jet flames. Then, the model is introduced in a turbulent flow simulation software. Three configurations are retained to quantify the level of prediction of this formulation: the D and F-Flames of Sandia and lifted jet flames of methane/air of Stanford. A good agreement is observed between experiments and simulations. The validity of this method is then demonstrated. (author)

  17. 基于PLC控制的航空碳-碳复合材料X射线数字成像检测装置的设计与研发%Development and Design on X-Ray Digital Imaging Detection Equipment of Aeronautic Carbon-carbon Composite Based on PLC Control

    Institute of Scientific and Technical Information of China (English)

    蔡建刚; 赵肖东; 陈兆兴; 陈明

    2013-01-01

    航空碳—碳复合材料X射线数字成像检测装置是供航空制造业中小型关键复合材料零部件X射线检测的设备.依据被检测产品的特点,该装置设计有前后、左右、上下六个自由度,可实现旋转、倾斜等运动形式.其传动系统采用步进电机和伺服电机驱动;谐波减速机、蜗杆减速机减速;滚动轴承支承、滚动直线导轨导向;滚珠丝杠、齿轮传动的方式.控制系统采用模块化结构的PLC控制,完成具体的运动执行控制.速度调节范围为0.1~3.0 m/min,定位误差≤0.2 mm,电机联动误差≤1 ms(一个PLC程序扫描周期),根据被检工件的检测要求实现了实时多角度、全位置X射线数字成像检测.%X-ray digital imaging detection device of aeronautic carbon-carbon composite is X-ray inspection equipment for the small and medium-sized pivotal composite material parts in the aeronautic manufacturing industry. In accordance with the characteristics of the detected product, six degrees of freedom of the front and back, left and right, up and down is designed, it can realize forms of movement of rotation and inclination. The transmission system adopts stepper motor and servo motor to drive, harmonic reducer and worm reducer to decelerate, rolling bearings to support and rolling linear guideway to guide, ball screw and gear to transmit. The control system uses a modular structure PLC control to complete the implementation of the specific motion control. In the device, the speed regulating range is form 0. 1 to 3.0m/min, the positioning error is less than 0.2mm, the motor linkage error is less than lms (a PLC program scan cycle). According to detection requirements of detected workpiece, real-time multi-angle and all-position X-ray digital imaging detection is achieved.

  18. Aeronautical Engineering: A Continuing Bibliography with Indexes (Supplement 216)

    Science.gov (United States)

    1987-08-01

    two types Conference on Aviation and Astronautics, 28th, Tel Aviv and Haifa, of air-film-cooling structures, six types of venturi -tube structures...design BERGER.@W U IT Noelnee mmwroen nw VIm ecp’e SK11117 design. p 474 A7-32450 Conllngenicl power for small tubo ~ht engne using Weighted no

  19. Send Student Interest Skyward!: Soaring Teaches Aeronautics Basics

    Science.gov (United States)

    Scarcella, Joe; Wallace, Art

    2011-01-01

    Gliders and sailplanes provide a great launching platform for teaching about technology and scientific principles. Soaring is technological innovation in action, using earth's natural resources for energy and endurance during flight. This article focuses on the basics of soaring, which educators can use to increase excitement and interest in the…

  20. Send Student Interest Skyward! Soaring Teaches Aeronautics Basics

    Science.gov (United States)

    Scarcella, Joe; Wallace, Art

    2011-01-01

    Gliders and sailplanes provide a great launching platform for teaching about technology and scientific principles. Soaring is technological innovation in action, using earth's natural resources for energy and endurance during flight. This article focuses on the basics of soaring, which educators can use to increase excitement and interest in the…

  1. Taking Flight: Using a Wind Tunnel to Teach Aeronautic Principles

    Science.gov (United States)

    Zembal-Saul, Carla; Huckans, John H.; Walker, Dean C.; Hershberger, Kimber; Kurz, Nathan A.; Reed, Diane; Cole, Milton W.

    2007-01-01

    Several teachers from State College (Pennsylvania) Area School District became intrigued with helping their students better understand the science associated with a unit on air and aviation. In particular, they observed that students often encountered difficulty with abstract flight concepts, such as lift, thrust, and drag. Content issues became…

  2. [Ionizing radiation in the aeronautics industry. Non-destructive testing].

    Science.gov (United States)

    La Verde, R; Travaglini, C

    1983-08-25

    The constant increase in the non-military use of nuclear energy in various fields induced this study of one particular field: the aero industry. Alitalia has been using gammagraphy and industrial metallography for nondestructive testing for over 20 years. Workers exposed to ionising radiations at work are protected by precisely detailed standards based on extremely rigorous national and international legislation. The health and protection of these workers is entrusted to a Company Doctor and a Qualified Specialist. The latter is thought to be indispensable since he is responsible for primary preventions as well as prompt diagnosis.

  3. 76 FR 12211 - Government/Industry Aeronautical Charting Forum Meeting

    Science.gov (United States)

    2011-03-04

    ..., from 8:30 a.m. to 5 p.m. at Advanced Management Technology, Inc. (AMTI), 1515 Wilson Boulevard... meet April 27 and 28, 2011 from 8:30 a.m. to 5 p.m. ADDRESSES: The meeting will be hosted by Advanced Management Technology, Inc. (AMTI), 1515 Wilson Boulevard, Arlington, VA 22209. FOR FURTHER...

  4. Software Acquisition Improvement in the Aeronautical Systems Center

    Science.gov (United States)

    2008-09-01

    selections, it’s the best value source selection theory…most bang for your buck 16 It is feasible, and should be done, but probably won’t 7 Yeah, I would...get awards, but nothing specific to software A. Yes 8 Yes, sometimes but amount not much and can be a morale booster A. Hard to quantify 18 Not that

  5. Air Force Academy Aeronautics Digest - Spring/Summer 1981.

    Science.gov (United States)

    1981-12-01

    technical culture in nec-primitive or anti-rational mytholoei(s. For example, during the 1930’s the American writer Henry Miller found expression for his...Mailer, and Henry Miller so astutely noted. To deal with it we must insure that students can program a computer and edit a paper on phys cs as well as

  6. Advancing Aeronautics: A Decision Framework for Selecting Research Agendas

    Science.gov (United States)

    2011-01-01

    assistance and support throughout this study. Jeff Hagen (RAND) and Mark Happel (then of RAND, now at Johns Hop- kins University Applied Physics...to results. NASA took this approach when President John F. Kennedy announced that the United States would pursue a program to land a man on the moon...Examples of improved engine concepts include variable bypass ratios, adaptive turbine glade pitches, and tradeoffs between noise and fuel efficiencies in

  7. SEE - Sight Effectiveness Enhancement. Results of the aeronautical evaluation

    DEFF Research Database (Denmark)

    Andersen, H.B.; Alapetite, Alexandre

    2006-01-01

    in Bordeaux, France. The simulator was equipped with a head-up display and the simulated environments specified and established in the project. Theevaluation has involved as test subjects six professional 737 airline pilots. The document describes objective and subjective measures of performance. The analysis...

  8. Surface Quality of Amilled Gamma Titaniumaluminide for Aeronautical Applications

    Directory of Open Access Journals (Sweden)

    Radkowski Grzegorz

    2014-06-01

    Full Text Available Gamma titanium aluminides are an interesting alternative for nickel, iron or cobalt matrix superalloys. Due to the advantageous strength properties at high temperatures they can successfully replace superalloys in applications such as high pressure compressor blades, low pressure turbine blades, high pressure compressor case, low pressure turbine case. Milling is one of the processes that can be applied in the forming elements made from this type of alloys for the aviation industry. Research included the selection of tool, the process kinematics and the range of milling gamma titanium aluminide (Ti-45Al-5Nb-0.2B-0.2C process parameters were carried out. Milling can be an effective method of forming of elements made of gamma TiAL in the range of processing parameters: vc = 20-70 m/min, ap = 0.3-0.7 mm, fz = 0.1- 0.45 mm/tooth. In the tests carried out the best results were obtained using a R300-016A20L- 08L milling cutter, S30T tool coating and in-cut milling.

  9. National Aeronautics and Space Administration Training Grant Supplement

    Science.gov (United States)

    DeWitt, Kenneth J.

    2005-01-01

    The following section summarizes the impact of the Ohio Space Grant Consortium (OSGC) in Ohio and to NASA over the last four-year period (February 1, 2001 to April 30, 2005) and highlights the important accomplishments of the consortium. The strength of the OSGC network of universities, community colleges, government agencies, industry, and outreach affiliates is well-established and is growing. The OSGC Consortium Management Structure was designed and remains committed to using the talents and diversity of everyone within this collaborative network, and operational policies and procedures are such that all consortium members are active contributors resulting in quality OSGC programs in research, education and service, while receiving a relatively small amount of NASA funds. The number of quality activities, both on- and off-campus, and collaborations/partnerships that OSGC has established with NASA and government agencies, state and local government, educational institutions, and private industry, has been impressive. Further desired university affiliate expansion requires additional funds. Diversity is shown in the OSGC 12-member Executive Committee by the presence of three campus representatives from Central State University, Wilberforce University, and The Ohio State University (two underrepresented minority, one female). One additional female campus representative (Cleveland State University) is currently on sabbatical leave and a valuable alternate member attends. Other additional female and underrepresented minority members are on the larger OSGC Advisory committee. All committee members participate fully in all consortium management and policy decisions. The OSGC Executive Committee strives to achieve and communicate a culture of trust, respect, teamwork, open communication, creativity, and empowerment. These programs have shown results and impact by their visibility and importance to Ohio and to NASA, resulting in strategic alliances created throughout Ohio. These alliances have improved over the last 4 years.

  10. 77 FR 71089 - Pilot Loading of Aeronautical Database Updates

    Science.gov (United States)

    2012-11-29

    ... restrictions, manpower and fuel consumption. If the aircraft is operated with an expired database, the pilot... location, the operator must absorb the costs of additional fuel consumption, and valuable time can be lost... meet shared challenges involving health, safety, labor, security, environmental, and other issues...

  11. Aeronautical Systems Division (AFSC) Program Management Resource Document.

    Science.gov (United States)

    1981-09-30

    MANAGEMENT Definition . Program management consists of the actions involved in developing and producing deliverable end items on time, within the...CONFIGURATION MANAGEMENT Definition . Configuration management is the formal process of identifying the functional and physical characteristics of

  12. The Literature of Aeronautics, Astronautics, and Air Power

    Science.gov (United States)

    1984-01-01

    Angeles: Floyd Clymer Publications, 1925, reissued, 1974), also called The Blue Book of American Airmen; the Writers’ Pro- gram of the Work Projects...record of the American space effort in Eyewitness to Space: Paintings and Drawings Related to the Apollo Mission to the Moon (New York: Abrams , 1971

  13. Aeronautical applications of steerable K/Ka-band antennas

    Science.gov (United States)

    Helmken, Henry; Prather, Horton

    1995-01-01

    The expected growth of wideband data and video transmission via satellite will press existing satellite Ku-band services and push development of the Ka-band region. Isolated ground based K/Ka-band terminals can experience severe fading due to rain and weather phenomena. However, since aircraft generally fly above the severe weather, they are attractive platforms for developing commercial K/Ka-band communication links.

  14. Aeronautical Engineering: A Continuing Bibliography with Indexes (Supplement 218)

    Science.gov (United States)

    1987-10-01

    Space Administration. CONFIGURATIONS Ames Research Center, Moffett Field, Calif. G. WEDEKIND and P. MANGOLD In AGARD Integrated Design V/STOL AND STOL...TIWARI, SURENDRA N. over finite wings p 556 A87-41630 p 617 A87-41230 Grid adaption for hypersonic flow VELKOFF, H. R. WEDEKIND , G. IAIAA PAPER 87-11691 p

  15. Web-Based Distributed Simulation of Aeronautical Propulsion System

    Science.gov (United States)

    Zheng, Desheng; Follen, Gregory J.; Pavlik, William R.; Kim, Chan M.; Liu, Xianyou; Blaser, Tammy M.; Lopez, Isaac

    2001-01-01

    An application was developed to allow users to run and view the Numerical Propulsion System Simulation (NPSS) engine simulations from web browsers. Simulations were performed on multiple INFORMATION POWER GRID (IPG) test beds. The Common Object Request Broker Architecture (CORBA) was used for brokering data exchange among machines and IPG/Globus for job scheduling and remote process invocation. Web server scripting was performed by JavaServer Pages (JSP). This application has proven to be an effective and efficient way to couple heterogeneous distributed components.

  16. CAD/CAM in the Brazilian aeronautical industry

    Science.gov (United States)

    Lampi, L. H.; Embraer, S. A.

    Features, applications and progress in the usage of CAD/CAM since 1980 by an aircraft manufacturer in Brazil are described. The system comprises 34 graphics work stations dedicated to structural design, lofting, electrical cable routing, finite element modeling and quality control. Standardized work methods have been devised to enhance productivity. Programs have been defined for finite element stress analysis and generating wiring diagrams. The computerized design capabilities have increased productivity for hole boring accuracy through work on digitized controllers. Psychological testing has been initiated to identify users who can adapt more easily to CAD/CAM utilization.

  17. Air Force Academy Aeronautics Digest, Spring/Summer 1980

    Science.gov (United States)

    1980-10-01

    is programmed in a high-level lan- guage using matrix notation, the actual programming is quite compact end ntreamlined. Netter (Ref. 7) described the...Methods for Determining Wind Speed and Direction." London: Her Majesty’s Stationery Office, 1971. 7. Netter , J. and W. Wasserman. Applied Linear

  18. Air Force Academy Aeronautics Digest - Fall/Winter 1980.

    Science.gov (United States)

    1981-05-01

    this is performed according to the procedure outlined by Netter and Wasserman (Ref. 4): First multiply each side of Eqn. (11) by the transpose of the...Wiley and Sons, 1976, p. 375. 4. Netter , J. and Wasserman, W. "Simple Linear Regression Model in Matrix Terms." Applied Linear Statistical Models

  19. National Aeronautics and Space Administration's (NASA) Automated Information Security Handbook

    Science.gov (United States)

    Roback, E.

    1991-01-01

    The NASA Automated Information Security Handbook provides NASA's overall approach to automated information systems security including discussions of such aspects as: program goals and objectives, assignment of responsibilities, risk assessment, foreign national access, contingency planning and disaster recovery, awareness training, procurement, certification, planning, and special considerations for microcomputers.

  20. Capacity Dimensioning for Aeronautical Communications in North Atlantic Corridor

    OpenAIRE

    Pirovano, Alain; Garcia, Fabien; Radzik, José

    2013-01-01

    http://www.kaconf.org/CD2013/papers/Ka_3/63.pdf; International audience; In the context of the Internet everywhere paradigm, aircraft passengers expect to get connectivity during flights. Several solutions based either on cellular networks in continental area or on satellite links have been designed and even deployed for some of them. But to face the increasing number of users and expected services, a migration to future satellite system such as Inmarsat's Ka band Global Xpress system have be...

  1. VFR Class B Graphics - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — These graphics are designed to increase safety and aid pilots in gaining situational awareness within existing and redesigned Class B areas. The graphic provides an...

  2. Aeronautical Decision Making for Student and Private Pilots.

    Science.gov (United States)

    1987-05-01

    14 percent of the accidents occurred during initial climb after takeoff. In addition to evaluating the previously mentioned landing items, pilots...should review the procedures for responding to an emergency during takeoff, e.g., an engine failure during ground run, liftoff and initial climb . These and...ris lt " *. , otf. rhte med ,iro of good de-, tion making in II in~z V J t pilot, pass,, gers and aircritt in good healti ind ck, ii !, n. ’.A f

  3. A New Approach to Multipath Mitigation in Aeronautical Telemetry

    Science.gov (United States)

    2011-06-23

    liz er de ci si on M M SE...eq ua liz er TR -S TB C TX a nt en na 1 TX a nt en na 2 r( t) y( t) y( kT b) y( kT b) h ∗ 1( − k T b ) h 1 (k T b ) h 2 (k T b... Jensen . Wideband mulitpath propagation for helicopter-to-ground telemetry links. In Proceedings of the International Telemetering Conference,

  4. Grand Canyon VFR Chart - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — The Federal Aviation Administration (FAA) digital-Visual Chart series is designed to meet the needs of users who require georeferenced raster images of a FAA Visual...

  5. Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics

    Science.gov (United States)

    Bushnell, Dennis M.

    2000-01-01

    This paper discusses Advanced Aircraft configurational approaches across the speed range, which are either enabled, or greatly enhanced, by clever Flow Control. Configurations considered include Channel Wings with circulation control for VTOL (but non-hovering) operation with high cruise speed, strut-braced CTOL transports with wingtip engines and extensive ('natural') laminar flow control, a midwing double fuselage CTOL approach utilizing several synergistic methods for drag-due-to-lift reduction, a supersonic strut-braced configuration with order of twice the L/D of current approaches and a very advanced, highly engine flow-path-integrated hypersonic cruise machine. This paper indicates both the promise of synergistic flow control approaches as enablers for 'Revolutions' in aircraft performance and fluid mechanic 'areas of ignorance' which impede their realization and provide 'target-rich' opportunities for Fluids Research.

  6. Use of nuclear data for space and aeronautic designs

    Energy Technology Data Exchange (ETDEWEB)

    Palau, M.C.; Carriere, Th. [Astrium ST, 78 - Les Mureaux (France); Buard, B.; Weulersse, C. [EADS IN, 92 - Suresnes (France); Saigne, F. [CEM2, 34 - Montpellier (France); Wrobel, F. [Nice Univ., LPES (France)

    2008-07-01

    Until recently, the effects of radiation environment on on-board electronics on launchers and aircraft had not been seriously taken into account. The situation has changed. And one of the most significant effects observed on on-board electronics is what we call Single Event Upset (SEU). This talk explains how the combination of electrical sensitivity of components and nuclear physics is important in the calculation of SEU rates, and emphasizes the aspects of nuclear physics useful to give the probability for a dangerous event to occur. Some circumvention methods will be rapidly identified. (authors)

  7. An Analysis of Total Quality Management in Aeronautical Systems Division

    Science.gov (United States)

    1991-09-01

    specifically designed to combat various types of waste. Concern over waste has existed for a long time; in the 1920s, Henry Ford dealt specifically with waste...costs approach infinity near perfect quality is a problem. "Infi- 3-25 0 1 UA VUALITY 0L COSTS o MINIMUM 0 TOTAL COSTo POINT C,. Lu (L INTERNAL I-.COST OF

  8. The Investigation and Countermeasures of Present Situation of University Network Public Opinion:Case Study of Nanjing University of Aeronautics and Astronautics%高校网络舆情现状调研及对策研究——以南京航空航天大学为例

    Institute of Scientific and Technical Information of China (English)

    赵文; 李珊; 余重远; 李瑞

    2011-01-01

    With the rapid development of Internet, universities has been closely related to public opinion of network, especially the campus network has its unique public opinion of network. The study selects Nanjing University of Aeronautics and Astronautics as case study, uses questionnaire survey to analyze public opinion. The goal is to understand the impact of web public opinion on the status of college students and the basic attitude of public opinion for the network .Based on the survey that focused on issues reflected in the questionnaire, the study gives recommendations of network problems and crises to the university.%在高速发展的今天,高校和网络舆情已经有着密不可分的关系,尤其是校园网络有着自己独特的网络舆情.文章选取南京航空航天大学为研究个案,采用问卷调查的方法,分析网络舆论对大学生的影响状况和大学生对于网络舆论的基本态度,针对调查结果集中反映的问题提出相应的建议,给高校应对网络舆论带来的问题和危机提供参考.

  9. 基于SWOT分析法的图书馆电子阅览室发展战略规划--以南昌航空大学图书馆为例%Strategic Development Planning of Library ’s Electronic Reading Room Based on SWOT Analysis---Taking the Library of Nanchang Aeronautical University as an Example

    Institute of Scientific and Technical Information of China (English)

    拱洁凡; 何小东

    2015-01-01

    ABSTRACT:Taking the library of Nanchang Aeronautical University as an example, this paper expounds the development status of university library’electronic reading room, and by using SWOT analysis method, probes into the problems existing in library’s electronic reading room, and based on this, establishes a SWOT matrix for library’s electronic reading room based on this, makes an analysis on various combinations, and puts forward the development strategy for library’s electronic reading room.%以南昌航空大学图书馆为例,阐述了高校图书馆电子阅览室的发展现状,并利用SWOT分析法,探讨了图书馆电子阅览室存在的问题,在此基础上构建了图书馆电子阅览室SWOT矩阵,对各种组合加以分析,提出了图书馆电子阅览室的发展战略。

  10. 基于NASA地球观测数据库的区域风电功率波动特性分析%Study on the Profiling of China's Regional Wind Power Fluctuation Using GEOS-5 Data Assimilation System of National Aeronautics and Space Administration of America

    Institute of Scientific and Technical Information of China (English)

    于大洋; 韩学山; 梁军; 宋曙光

    2011-01-01

    In China, inadequate historical wind data hinders the profiling of wind power fluctuation at the regional level, which is the fundamental work for the wind power integration. This paper proposes a method to assess the seasonal and diurnal wind power patters based on the wind speed data from the National Aeronautics and Space Administration (NASA) Goddard Earth Observing System Model, Version 5 Data Assimilation System (GEOS-5 DAS). The Gipe formula is applied to get the vertical distribution of the wind speed. The wind speed is transformed into the electric power according to the power curve of Vestas V90-2.0MW turbine. A quantitative analysis is made for six wind power bases in China to present the difference of seasonal wind power patters and the regional correlations of hourly wind power patters. The method and results provide the basis for the regional wind power scheduling and dispatching.%针对大范围和长期风速观测网络不完善、风资源数据缺乏的问题,提出利用美国航天局(NASA)Goddard地球观测系统数据同化系统的版本5(GEO-5 DAS)的全球风速数据,对国内大范围风电功率波动进行评估的方法.根据GEOS-5 DAS的50 m高度风速和Gipe公式得到风速的垂直分布,按照Vestas V90-2.0 Mw风电机组的功率特性曲线将风速转化为风电功率,得到不同时间尺度下的容量因数曲线.对中国正在建设的6个千万千瓦级风电基地的季节性风电功率波动、小时功率波动及其季节性差异和地域相关性进行了定量分析.所提出的分析方法和结果为区域风电科学规划和优化调度提供了科学的依据.

  11. Avaliações térmica e reológica da matriz termoplástica PEKK utilizada em compósitos aeronáuticos Thermal and rheological evaluation of PEKK thermoplastic matrix for aeronautical application

    Directory of Open Access Journals (Sweden)

    Rogério L. Mazur

    2008-09-01

    resistance combined with its low density make PEKK an attractive option for a variety of applications in aerospace and aeronautical field. The aim of the present work is to analyze the influence of the thermal and rheological parameters of PEKK using the techniques Fourier Transform InfraRed (FT-IR, differential scanning calorimetry (DSC, thermogravimetry (TG and rheology, in the definition of processing thermal cycle to be utilized with the hot compression molding of thermoplastic composites. The results obtained from the thermal and rheological analyses showed that PEKK has an attractive balance of properties, such as a high transition temperature (Tg = 153-156 °C and of being able to be processed at a moderate temperature, between the melting (310-325 °C and degradation (352-366 °C temperatures, mainly when compared with other polymers, including PEEK (polyether ether ketone, PEI (Polyetherimide and PPS (polyphenylene sulfide. From these results, it was possible to establish appropriate thermal and rheological parameters to be used in hot compression molding of advanced polymeric laminates.

  12. Avaliação da temperatura de transição vítrea de compósitos poliméricos reparados de uso aeronáutico Evaluation of glass transition temperature of the repaired polymeric composites of aeronautical use

    Directory of Open Access Journals (Sweden)

    Jane M. F. de Paiva

    2006-03-01

    lay-up process used in aeronautical industry. Afterwards, simulated damages, scarf type, were made and overlapping layers of F155 epoxy resin prepregs repaired them. The DMTA curves show the effects of combination of different systems resins on the Tg values and, consequently, on the service temperature of the repaired laminate. The used repairing material (based on epoxy resin F155 and on epoxy adhesive film FM73 decreased the Tg of the repaired laminates in approximately 30 °C for the carbon and glass laminates. The conditioning of aramide laminate under elevated humidity and temperature provoked a more decrease of the Tg (reduction of approximately 40 °C. The Tg reduction for the repaired laminates is attributed to the adhesive film migration into the F155 resin system during the cure process and also to the resin plasticization by water diffusion during the hygrothermal conditioning. The Tg reduction leads to a decrease of the service temperature of the repaired polymeric composite.

  13. 从多功能空间设计看现代高校图书馆建设--以南京航空航天大学将军路校区图书馆为例%Discussion on the Construction of Modern University Library from the Design of Multi-functional Space---Case Study of Jiangjun Road Campus Library of Nanjing University of Aeronautics & Astronautics

    Institute of Scientific and Technical Information of China (English)

    魏翠娟

    2015-01-01

    ABSTRACT:Taking Jiangjun Road Campus Library of Nanjing University of Aeronautics&Astronautics as an example, this paper expounds the overall construction of this library, and introduces in detail its multi-functional space including the collection and study space, digital resource space, academic research space, leisure and social space, activity space and self-service space in order to provide the reference and enlightenment for the construction of university library.%以南京航空航天大学将军路校区图书馆为例,阐述了该馆的整体建设情况,对其多功能空间(藏书及学习空间、电子资源空间、学术研讨空间、休闲社交空间、活动空间、自助服务空间)进行了详细介绍,以期为现代大学图书馆建设提供参考和启示。

  14. 78 FR 10247 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-02-13

    ....65 feet to the South right of line of Debra Lane as dedicated by said J.R. Willen Wheeling Estates... Seconds East, an ARC distance of 598.51 feet to the North Right of Way line of Debra Lane as dedicated by... 17 Seconds West along said Debra Lane, A distance of 682.70 feet to the West line of said...

  15. L-Band Digital Aeronautical Communications System Engineering - Initial Safety and Security Risk Assessment and Mitigation

    Science.gov (United States)

    Zelkin, Natalie; Henriksen, Stephen

    2011-01-01

    This document is being provided as part of ITT's NASA Glenn Research Center Aerospace Communication Systems Technical Support (ACSTS) contract NNC05CA85C, Task 7: "New ATM Requirements--Future Communications, C-Band and L-Band Communications Standard Development." ITT has completed a safety hazard analysis providing a preliminary safety assessment for the proposed L-band (960 to 1164 MHz) terrestrial en route communications system. The assessment was performed following the guidelines outlined in the Federal Aviation Administration Safety Risk Management Guidance for System Acquisitions document. The safety analysis did not identify any hazards with an unacceptable risk, though a number of hazards with a medium risk were documented. This effort represents a preliminary safety hazard analysis and notes the triggers for risk reassessment. A detailed safety hazards analysis is recommended as a follow-on activity to assess particular components of the L-band communication system after the technology is chosen and system rollout timing is determined. The security risk analysis resulted in identifying main security threats to the proposed system as well as noting additional threats recommended for a future security analysis conducted at a later stage in the system development process. The document discusses various security controls, including those suggested in the COCR Version 2.0.

  16. L-Band Digital Aeronautical Communications System Engineering - Concepts of Use, Systems Performance, Requirements, and Architectures

    Science.gov (United States)

    Zelkin, Natalie; Henriksen, Stephen

    2010-01-01

    This NASA Contractor Report summarizes and documents the work performed to develop concepts of use (ConUse) and high-level system requirements and architecture for the proposed L-band (960 to 1164 MHz) terrestrial en route communications system. This work was completed as a follow-on to the technology assessment conducted by NASA Glenn Research Center and ITT for the Future Communications Study (FCS). ITT assessed air-to-ground (A/G) communications concepts of use and operations presented in relevant NAS-level, international, and NAS-system-level documents to derive the appropriate ConUse relevant to potential A/G communications applications and services for domestic continental airspace. ITT also leveraged prior concepts of use developed during the earlier phases of the FCS. A middle-out functional architecture was adopted by merging the functional system requirements identified in the bottom-up assessment of existing requirements with those derived as a result of the top-down analysis of ConUse and higher level functional requirements. Initial end-to-end system performance requirements were derived to define system capabilities based on the functional requirements and on NAS-SR-1000 and the Operational Performance Assessment conducted as part of the COCR. A high-level notional architecture of the L-DACS supporting A/G communication was derived from the functional architecture and requirements.

  17. Computational Modeling of the Dielectric Barrier Discharge (DBD) Device for Aeronautical Applications

    Science.gov (United States)

    2006-06-01

    Dielectric Barrier Discharge The Dielectric Barrier Discharge (DBD) device has been put to use since 1857 when Werner von Siemens used to produce...x y s t s t x y x ys t s t s t s t x y x y x yn S L t nx + − − Γ − Γ = − − Δ + Δ (18) and 1 1 2 2 , , , , ,, , , , , 1 , 1...driven flux and the thermal flux were oppositely directed. ( ), , , , 1s t s t s t s tadjacent Scharfetter Gummel thermal adjacenttn S L nx − − Δ = Γ

  18. Unlimited Horizons: Design and Development of the U-2. [NASA Aeronautics Book Series

    Science.gov (United States)

    Merlin, Peter W.

    2015-01-01

    This book describes the creation, history, design, and research value of the U-2 program. It also describes the involvement of NACA, as a cover story, and the later use by NASA of these aircraft as environmental research platforms.

  19. 76 FR 72240 - Twenty-Seventh Meeting: RTCA Special Committee 206: Aeronautical Information and Meteorological...

    Science.gov (United States)

    2011-11-22

    .../Roadmap--SG3 Chairmen Discuss Proposed TOR Changes Final Review and Comment (FRAC): Operational Services... dates Approve proposed TOR changes Decision to release the ConUse document for FRAC process Decision...

  20. 76 FR 54526 - 26th Meeting: RTCA Special Committee 206: Aeronautical Information and Meteorological Data Link

    Science.gov (United States)

    2011-09-01

    ... Deliverables in TOR and potential changes. Discuss the certification and liability issues surrounding the use... Dates. Discuss Status of Deliverables in TOR and potential changes. Decision to release DO-267A...

  1. 77 FR 3030 - Twenty-Eighth Meeting: RTCA Special Committee 206: Aeronautical Information and Meteorological...

    Science.gov (United States)

    2012-01-20

    ... proposed TOR changes ConUse Review February 7, 2012 ConUse Review February 8, 2012 SG1, SG2, and SG3... presentation selection process Approve advisory and normal definitions Approve proposed TOR changes and new...

  2. 77 FR 20688 - 29th Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data Link...

    Science.gov (United States)

    2012-04-05

    ... Status. Discuss previously proposed TOR changes and DO-252 Revision. Discuss TOR changes for the June PMC... release to the PMC. Agree upon TOR changes for June PMC meeting. Other business. Adjourn--1...

  3. 76 FR 28626 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model...

    Science.gov (United States)

    2011-05-18

    ... and 20,000 flight hours for Hi-Tigues in cold-worked holes). LM Aero stated that the installation...-case basis to address cold-worked holes and installation of Hi-Tigue fasteners in affected areas of the...-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590....

  4. Solid Lubrication by Multiwalled Carbon Nanotubes in Air and in Vacuum for Space and Aeronautics Applications

    Science.gov (United States)

    Miyoshi, Kazuhisa; Street, Kenneth W., Jr.; Andraws, Rodney; Jacques, David; VanderWal, Randy L.; Sayir, Ali

    2005-01-01

    To evaluate recently developed aligned multiwalled carbon nanotubes (MWNTs) and dispersed MWNTs for solid lubrication applications, unidirectional sliding friction experiments were conducted with 440 C stainless steel balls and hemispherical alumina-yttria stabilized zirconia pins in sliding contact with the MWNTs deposited on quartz disks in air and in vacuum. The results indicate that MWNTs have superior solid lubrication friction properties and endurance lives in air and vacuum under dry conditions. The coefficient of friction of the dispersed MWNTs is close to 0.05 and 0.009 in air and in vacuum, respectively, showing good dry lubricating ability. The wear life of MWNTs exceeds 1 million passes in both air and vacuum showing good durability. In general, the low coefficient of friction can be attributed to the combination of the transferred, agglomerated patches of MWNTs on the counterpart ball or pin surfaces and the presence of tubular MWNTs at interfaces.

  5. 75 FR 16901 - Thirteenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security...

    Science.gov (United States)

    2010-04-02

    ...). SUMMARY: The FAA is issuing this notice to advise the public of a meeting of EUROCAE WG-72: RTCA Special...: Introduction/review of the previous MoM/ Report about publications/Approval of the meeting agenda. 09h20 to... processes in relation to the planned releases for this year/early next--verify publication schedule....

  6. Sectoral Innovation Foresight. Space and Aeronautics Sectors. Final Report. Task 2

    NARCIS (Netherlands)

    Brandes, F.; Poel, M.

    2011-01-01

    The European aerospace industry is world leader in large civil aircraft, business jets and helicopters, aero-engines and defence electronics. The sector in Europe is dominated by a small number of large firms highly concentrated in the UK, France and Germany. It is a mature market focusing on increm

  7. 75 FR 81678 - Aeronautics Science and Technology Subcommittee; Committee on Technology; National Science and...

    Science.gov (United States)

    2010-12-28

    ... conjunction with the 49th AIAA Aerospace Sciences Meeting at the Orlando World Center Marriott, 8701 World... Ballroom A. Information regarding the 49th AIAA Aerospace Sciences Meeting is available at the: http://www.aiaa.org Web site. Note: Persons solely attending this ASTS public meeting do not need to register...

  8. 75 FR 36722 - Aeronautics Science and Technology Subcommittee; Committee on Technology; National Science and...

    Science.gov (United States)

    2010-06-28

    ... meeting will be held in conjunction with the 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit... p.m. to 4:30 p.m., in Room 201. Information regarding the 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit is available at the: http://www.aiaa.org Web site. Note: Persons solely attending...

  9. 77 FR 47913 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Southern Illinois Airport...

    Science.gov (United States)

    2012-08-10

    ... location by appointment or at the Southern Illinois Airport, P.O. Box 1086, Carbondale, Illinois 62903... South 02 Degrees 15 Minutes 44 Seconds West for a distance of 166.04 feet, and an arc distance of 166.05... 14 Degrees 26 Minutes 02 Seconds East for a distance of 156.40 feet, and an arc distance of...

  10. 77 FR 63275 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

    Science.gov (United States)

    2012-10-16

    .... Discussion On July 8, 2005, we issued AD 2005-15-01, Amendment 39-14191 (70 FR 42262, July 22, 2005), for all...-15-01, Amendment 39-14191 (70 FR 42262, July 22, 2005), we have received reports of small cracks... (outboard). Relevant Service Information AD 2005-15-01, Amendment 39-14191 (70 FR 42262, July 22,...

  11. 76 FR 58416 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L...

    Science.gov (United States)

    2011-09-21

    ... proposed AD. Discussion We previously issued AD 94-05-01, Amendment 39-8839 (59 FR 10275, March 4, 1994), and AD 2000-21-01, Amendment 39-11933 (65 FR 62994, October 20, 2000), which require modifications to... (59 FR 10275, March 4, 1994), and AD 2000-21-01, Amendment 39-11933 (65 FR 62994, October 20,...

  12. 76 FR 48049 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L...

    Science.gov (United States)

    2011-08-08

    ... proposed AD. Discussion On December 5, 1995, we issued AD 95-20-04 R1, Amendment 39-9454 (60 FR 63414... removes an SSD that has been addressed by AD 99-08-20, amendment 39-11128 (64 FR 18324, April 14, 1999... the NPRM for AD 95-20-04, Amendment 39-9382 (60 FR 51713, October 3, 1995) we stated that as...

  13. Risk management. National Aeronautics and Space Administration (NASA). Interim rule adopted as final with changes.

    Science.gov (United States)

    2000-11-22

    This is a final rule amending the NASA FAR Supplement (NFS) to emphasize considerations of risk management, including safety, security (including information technology security), health, export control, and damage to the environment, within the acquisition process. This final rule addresses risk management within the context of acquisition planning, selecting sources, choosing contract type, structuring award fee incentives, administering contracts, and conducting contractor surveillance.

  14. 76 FR 82106 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

    Science.gov (United States)

    2011-12-30

    ... September 21, 2011 (76 FR 58416). That NPRM proposed to require repetitive inspections for cracking of the... opportunity to participate in developing this AD. We received no comments on the NPRM (76 FR 58416, September... Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in...

  15. The Education of Future Aeronautical Engineers: Conceiving, Designing, Implementing and Operating

    Science.gov (United States)

    Crawley, Edward F.; Brodeur, Doris R.; Soderholm, Diane H.

    2008-01-01

    This paper will outline answers to the two central questions regarding improving engineering education: (1) What is the full set of knowledge, skills, and attitudes that engineering students should possess as they leave the university, and at what level of proficiency?; and (2) How can we do better at ensuring that students learn these skills? The…

  16. 77 FR 20522 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

    Science.gov (United States)

    2012-04-05

    ... listed in this AD as of November 2, 1995 (60 FR 51713, October 3, 1995). ADDRESSES: For service..., Amendment 39-9454 (60 FR 63414, December 11, 1995). That AD applies to the specified products. The NPRM published in the Federal Register on August 8, 2011 (76 FR 48049). That NPRM proposed to continue to...

  17. Rheology and mechanics of polyether(ether)ketone - Polyetherimide blends for composites in aeronautics

    Science.gov (United States)

    Rosa, Mattia; Grassia, Luigi; D'Amore, Alberto; Carotenuto, Claudia; Minale, Mario

    2016-05-01

    In the present work rheological and mechanical properties of PEEK-PEI blends were investigated. Besides the pure components, blends with PEI concentration ranging from 10% to 90% in mass were considered. Oscillatory experiments in controlled atmosphere were conducted at different frequencies and temperatures. The frequency responses at different temperatures allowed using the TTS principle to reconstruct the master curves. All systems showed a shear thinning behavior and a flux index increasing with the percentage of PEI. The zero-shear viscosity was computed with the implementation of the Cross model and showed a decreasing behavior with the percentage of PEI. The relaxation time estimated from the crossover value of storage and loss moduli didn't change significantly with blend composition, suggesting the non-sensibility of the elasticity of the system. Lastly, tensile tests were executed to investigate the dependence of Young modulus in the different blends.

  18. Conceptual Design and Cost Estimate of a Subsonic NASA Testbed Vehicle (NTV) for Aeronautics Research

    Science.gov (United States)

    Nickol, Craig L.; Frederic, Peter

    2013-01-01

    A conceptual design and cost estimate for a subsonic flight research vehicle designed to support NASA's Environmentally Responsible Aviation (ERA) project goals is presented. To investigate the technical and economic feasibility of modifying an existing aircraft, a highly modified Boeing 717 was developed for maturation of technologies supporting the three ERA project goals of reduced fuel burn, noise, and emissions. This modified 717 utilizes midfuselage mounted modern high bypass ratio engines in conjunction with engine exhaust shielding structures to provide a low noise testbed. The testbed also integrates a natural laminar flow wing section and active flow control for the vertical tail. An eight year program plan was created to incrementally modify and test the vehicle, enabling the suite of technology benefits to be isolated and quantified. Based on the conceptual design and programmatic plan for this testbed vehicle, a full cost estimate of $526M was developed, representing then-year dollars at a 50% confidence level.

  19. In-Plane Moire Optical Processing at ARL (Aeronautical Research Laboratories)

    Science.gov (United States)

    1987-07-01

    work is copyright. Apart from any fair dealing for the purpose of study, research, criticism or review, as permitted under the Copyright Act, no part ...future as part of a calibration procedure for automatic fringe analysis. A movement of one grating pitch of the retrrence grating will reproduce the...TEST RESULTS 7.1 The J-integral specimen A Hounsfield Tensometer was used to apply tensile load to the J-integral specimen through the bolt holes

  20. Case Meetings for Teaching English for Specific Academic Purposes in a Tertiary Aeronautical Engineering Programme

    Science.gov (United States)

    Tatzl, Dietmar

    2015-01-01

    This article presents an innovative adaptation of the case method to teaching English for specific academic purposes. Widespread in its traditional form in various content disciplines, the case method bears the potential for truly student-centred language instruction. The current application transforms learners from case analysts to case authors…

  1. 76 FR 22311 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model...

    Science.gov (United States)

    2011-04-21

    ..., there was a full- ] scale fatigue test performed on military airplanes based on military usage. The initial and recurring inspection intervals were based on a typical military transport usage and were... (75 FR 13695). That NPRM proposed to require repetitive eddy current inspections to detect cracks...

  2. Space Research Data Management in the National Aeronautics and Space Administration

    Science.gov (United States)

    Ludwig, G. H.

    1986-01-01

    Space related scientific research has passed through a natural evolutionary process. The task of extracting the meaningful information from the raw data is highly involved and will require data processing capabilities that do not exist today. The results are presented of a three year examination of this subject, using an earlier report as a starting point. The general conclusion is that there are areas in which NASA's data management practices can be improved and recommends specific actions. These actions will enhance NASA's ability to extract more of the potential data and to capitalize on future opportunities.

  3. National Aeronautics and Space Administration Marshall Space Flight Center Space Transportation Directorate Risk Management Implementation Program

    Science.gov (United States)

    Duarte, Luis Alberto; Kross, Denny (Technical Monitor)

    2001-01-01

    The US civil aerospace program has been a great contributor to the creation and implementation of techniques and methods to identify, analyze, and confront risk. NASA has accomplished mission success in many instances, but also has had many failures. Anomalies have kept the Agency from achieving success on other occasions, as well. While NASA has mastered ways to prevent risks, and to quickly and effectively react and recover from anomalies or failures, it was not until few years ago that a comprehensive Risk Management process started being implemented in some of its programs and projects. A Continuous Risk Management (CRM) cycle process was developed and has been promoted and used successfully in programs and projects across the Agency.

  4. Services provided in support of the planetary quarantine requirements of the National Aeronautics and Space Administration

    Science.gov (United States)

    Favero, M. S.

    1972-01-01

    Heat studies with the highly resistant bacterial spore isolated from Cape Kennedy soil were continued, and the D130C was determined. The interior surfaces of the command module of the Apollo 17 spacecraft were studied for microbial contamination during assembly and testing. The thermal resistance of naturally occurring airborne bacterial spores was determined, using the heating times of 2, 4, 6, and 8 hr. at 125 C. The evaluation of a terminal sterilization process for unmanned lander spacecraft is also continuing.

  5. Terminal Procedures Publication/Airport Diagrams - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — The U.S. Terminal Procedure Publications (TPPs) is a 26 volume set of printed paper books containing Instrument Approach Procedure charts (IAP), Departure Procedure...

  6. Properties of welded joints in laser welding of aeronautic aluminum-lithium alloys

    Science.gov (United States)

    Malikov, A. G.; Orishich, A. M.

    2017-01-01

    The work presents the experimental investigation of the laser welding of the aluminum-lithium alloys (system Al-Mg-Li) and aluminum alloy (system Al-Cu-Li) doped with Sc. The influence of the nano-structuring of the surface layer welded joint by the cold plastic deformation method on the strength properties of the welded joint is determined. It is founded that, regarding the deformation degree over the thickness, the varying value of the welded joint strength is different for these aluminum alloys.

  7. The reduction of the National Aeronautics and Space Administration plates at the New Mexico University

    Science.gov (United States)

    Haas, W. H.

    1971-01-01

    A method of reducing GEOS satellite plates is described. The catalog positions of stars, whose images were measured, are updated to the time of the photographic observation. The plate constants are used to compute the positions of the seven (or fewer) flashing light images which were measured. There are corrected for refraction, parallax, and radial and decentering lens distortions. With sidereally tracking cameras, the exterior orientation is further corrected to the time of the particular flash, and the change of refraction with time is allowed for. First and second differences and standard deviations and covariances for the flashing light images are developed as a measure of accuracy.

  8. The National Aeronautics and Space Administration Semiannual Report to the Congress

    Science.gov (United States)

    1959-03-31

    Carolina) R. Walter Riehlman (New York) Leonard G Wolf (Iowa) Joseph E. Karth (Minnesota) Ken Hechler (West Virginia) Emilio Q. Daddario (Connecticut...KEITH GLENNAN WILBER M. BRUCKER Administrator, NASA Secretary of the Army - 87 - APPENDIX I COOPERATIVE AGREEMENT ON ARMY ORDNANCE MISSILE COMMAND Between...NASA, in implementation of this agreement. Date: 3 December 1958 Washington, D. C. (SIGNED) (SIGNED) T. KEITH GLENNAN WILBER M. BRUCKER Administrator

  9. North Atlantic IFR Route Planning Chart GEO-TIFF - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — North Atlantic Route Chart is designed for FAA Controllers to monitor transatlantic flights, this 5-color chart shows oceanic control areas, coastal navigation aids,...

  10. North Atlantic IFR Route Planning Chart PDF File - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — North Atlantic Route Chart is designed for FAA Controllers to monitor transatlantic flights, this 5-color chart shows oceanic control areas, coastal navigation aids,...

  11. Aeronautics Education, Research, and Industry Alliance (AERIAL) Year 2 Report and Year 3 Proposal

    Science.gov (United States)

    Bowen, Brent D.; Box, Richard C.; Fink, Mary M.; Gogos, George; Lehrer, Henry R.; Narayanan, Ram M.; Nickerson, Jocelyn S.; Tarry, Scott E.; Vlasek, Karisa D.

    2003-01-01

    The UNO Aviation Institute Monograph Series began in 1994 as a key component of the education outreach and information transfer missions of the Aviation Institute and the NASA Nebraska Space Grant & EPSCoR Programs. The series is an outlet for aviation materials to be indexed and disseminated through an efficient medium. Publications are welcome in all aspects of aviation. Publication formats may include, but are not limited to, conference proceedings, bibliographies, research reports, manuals, technical reports, and other documents that should be archived and indexed for future reference by the aviation and world wide communities.

  12. Finishing aeronautical planetary herringbone gear wheels in container vibrating smoothing machine

    Directory of Open Access Journals (Sweden)

    Jacek MICHALSKI

    2015-12-01

    Full Text Available The paper presents the technological process of abrasive-chemical machining wheel bearing surface of the cylindrical herringbone gears planetary gear in vibrating container smoothing machine according to Isotropic Finishing ISF® technology of the REM Chemicals Inc. company. Gear wheels are made of stainless Pyrowear 53 and subjected to carburizing, hardening, cold working and low tempering. The change in value of deviation indicators for the kinematic accuracy, smoothness and geometric structure of the machined surfaces of the gear teeth after smoothing compared with the contoured grinding were analyzed. The findings are different a characteristic performance on the surface of the tooth side along the outline, especially with a higher value at the head of the tooths. This creates a need for appropriate modification of the lateral surface of the teeth in the process of contoured grinding. The results of the mechanical strength of the samples gear wheel after the smoothing process and evaluating the hydrogen embrittlement are presented.

  13. 75 FR 5173 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Indianapolis International Airport...

    Science.gov (United States)

    2010-02-01

    ... feet along an arc to the right having a radius of 661.18 feet and subtended by a long chord having a... Minnesota Street Northeasterly 26.69 feet along an arc to the right having a radius of 355.00 feet and... along an arc to the left having a radius of 445.00 feet and subtended by a long chord having a...

  14. 77 FR 30584 - Thirtieth Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data...

    Science.gov (United States)

    2012-05-23

    ... report SG3 report SAE G-10 AI ARP Briefing to SC-206 Plenary 12:30 p.m. Review ConUse Changes 12 June.... Closing Plenary SG1 report SG2 report Decision to approve the ConUse document for release to the PMC...

  15. Evaluating Aircrew and Maintainer Warfighter Performance in Aeronautical Systems using Mission-Oriented Measures of Effectiveness

    Science.gov (United States)

    2001-02-01

    performed work on this project under a subcontract with Metrica , Incorporated. This 3-year project was performed initially for the Air Force Armstrong...and the remaining portion was conducted under prime contract F41624-97-5030 with Metrica , Incorporated and their subcontract to UDRI, 4050-003-01

  16. Calendar of Selected Aeronautical and Space Meetings (Calendrier des Manifestations Aeronautiques et Spatiales (Selection))

    Science.gov (United States)

    1989-01-01

    Luxembourg BR Brazil ME Mexico BU Bulgaria MO Monaco CA Canada NL Netherlands CH Switzerland NO Norway CI Ivory Coast NZ New Zealand CN China OS...OH 440t73. Tel. (2 16) 338-5 151 US ASMA Aerospace Medical Association: National Airport. Washington. 1)C 2000))1-4977, Tel. (7013) 892-2 24)) US ASME...Space Nuclear Power Studies: Chemical and Nuclear Engineering Dept.. University of New Mexico , Albuquerque, NM 87131 US ISVR Institute of Sound and

  17. Ultrasonic characterization of delamination in aeronautical composites using noncontact laser generation and detection.

    Science.gov (United States)

    Sun, Guangkai; Zhou, Zhenggan; Chen, Xiucheng; Wang, Jie

    2013-09-10

    The characterization of delamination in composite plates with ultrasonic waves generated and detected by lasers is presented. Composite materials have become one of the most important structural materials in the aviation industry because of their excellent mechanical properties, such as high specific stiffness and antifatigue. This paper reports a new application of the laser ultrasonic technique to perform nondestructive detection of carbon-fiber-reinforced plastic (CFRP) and continuous-fiber-reinforced ceramic matrix composites (CFCCs) containing artificial internal defects, based on propagation characteristic of ultrasonic waves generated by pulse laser with a wavelength of 1064 nm and pulse duration of 10 ns. A laser interferometer based on two-wave mixing is used to measure ultrasonic wave signals. The main advantage of this technique over conventional ultrasonic testing techniques is the ability to carry out detection without using coupling agents. The research results prove that the laser ultrasonic technique is effective for the detection of internal defects in both CFRP and CFCC composite components, which should promote and expand the application of the technique in the aviation industry.

  18. 78 FR 41314 - Review of Foreign Ownership Policies for Common Carrier and Aeronautical Radio Licensees

    Science.gov (United States)

    2013-07-10

    ... Universal Licensing System (ULS) (for wireless licensees) or IBFS (for satellite radio licensees). 22. The... ``small business,'' ``small organization,'' and ``small governmental jurisdiction.'' \\4\\ In addition,...

  19. 78 FR 38091 - Airworthiness Criteria: Proposed Airship Design Criteria for Lockheed Martin Aeronautics Model...

    Science.gov (United States)

    2013-06-25

    ..., to the address specified above. All communications received on or before the closing date for... document ``FAA-P-8110-2, Airship Design Criteria (ADC),'' dated November 2, 1987 with Change 1, dated July... airships in the United States for many years. The ADC is inadequate for an aircraft with the size...

  20. Research on the Aeronautical Static Inverter%航空静止变流器技术

    Institute of Scientific and Technical Information of China (English)

    王帮亭; 郑建

    2011-01-01

    静止变流器是飞机电源系统的核心组成部分,它不仅直接关系到飞机的飞行安全,同时也是决定航空电源系统技术水平的主要因素之一。文中主要对静止变流器的实现方法进行了研究,提出一种双Buck逆变器拓扑结构。该方法采用一种单相双降压式电路拓扑,不存在桥臂直通,开关管体二极管不参与工作,不存在体二极管反向恢复损耗大的问题,效率高、可靠性高。通过仿真实验验证了提出的静止变流器拓扑结构的特性%Static Inverter is a key component of aircraft electrical power system(EPS).It is not only associated with the flight safety,but also a key element which affects the technology level of aircraft EPS.This paper focuses on the research on the realization methodology of the static inverter,and presents a double Buck inverter topology for the static inverter.A single phase double Buck circuit topology is used,which can eliminate the short circuit in one side of bridge.The diode attached to the switching device will not be involved in the operation.Therefore,there will be no large power loss of the switching device.The efficiency and reliability of the static inverter will be higher.The presented topology for the static inverter has been verified by simulation results

  1. 77 FR 5420 - Airworthiness Directives; Aeronautical Accessories Inc. High Landing Gear Aft Crosstube Assembly

    Science.gov (United States)

    2012-02-03

    ... each aft crosstube for a crack. If there are no cracks, thereafter at specified intervals, priming and... crosstube for a crack. If there are no cracks, priming and painting the inspection area. If there is a crack... justifies making a regulatory distinction; and 4. Will not have a significant economic impact, positive...

  2. 77 FR 27663 - Airworthiness Directives; Aeronautical Accessories, Inc. High Landing Gear Forward Crosstube...

    Science.gov (United States)

    2012-05-11

    ... justifies making a regulatory distinction; and 4. Will not have a significant economic impact, positive or... before priming and painting the inspection areas. (3) Thereafter, at intervals not to exceed 200...

  3. 77 FR 67261 - Airworthiness Directives; Aeronautical Accessories, Inc., High Landing Gear Forward Crosstube...

    Science.gov (United States)

    2012-11-09

    ... justifies making a regulatory distinction; and (4) Will not have a significant economic impact, positive or... before priming and painting the inspection areas. (3) Thereafter, at intervals not to exceed 200...

  4. Remote sensing of land processes: Sponsored programs of study by the National Aeronautics and Space Administration

    Science.gov (United States)

    Asrar, G.; Wickland, D. E.; Baltuck, M.; Ruzek, M. J.; Murphy, R. E.

    1988-01-01

    The NASA Land Processes Program consists of four interrelated disciplines which support studying the terrestrial geology, ecology, hydrology, and remote sensing science. The first three represent the space based components of classical science disciplines, while the last discipline is the study of the physics, biology, and chemistry of the land surface as it relates to the interaction of electromagnetic energy with the land surface.

  5. An Analysis of an R&D Program Selection Process at the Aeronautical Systems Division.

    Science.gov (United States)

    1980-09-01

    interrelationships with respect to both value contribution and resource utilization [Baker and Freeland, 1975:1165]." Aaker and Tyebjee have suggested a...function and to the resource constraints ( Aaker and Tyebjee, 1978:30- 36). The first type of interdependency is due to overlap in project resource...organization ( Aaker and Tyebjee, 1978:30). Several major criteria are common to all of the recommended evaluation criteria in the literature. All

  6. Research and Development Project Selection Methods at the Air Force Wright Aeronautical Laboratories.

    Science.gov (United States)

    1985-09-01

    680). Aaker and Tyebee. 1978. The authors constructed a model that dealt with the selection of interdependent R&D projects. The model covers three...Response Linear Programming 1 Goal Programing 5 Multiple Objective 4 Chance Constrained Prog 0 Other 11 63 Bibliography 1. Aaker , David A. and Tyzoon T

  7. NASA University Research Centers Technical Advances in Education, Aeronautics, Space, Autonomy, Earth and Environment

    Science.gov (United States)

    Jamshidi, M. (Editor); Lumia, R. (Editor); Tunstel, E., Jr. (Editor); White, B. (Editor); Malone, J. (Editor); Sakimoto, P. (Editor)

    1997-01-01

    This first volume of the Autonomous Control Engineering (ACE) Center Press Series on NASA University Research Center's (URC's) Advanced Technologies on Space Exploration and National Service constitute a report on the research papers and presentations delivered by NASA Installations and industry and Report of the NASA's fourteen URC's held at the First National Conference in Albuquerque, New Mexico from February 16-19, 1997.

  8. Improvement of the military academy education system for aeronautics students using the flying laboratory

    Directory of Open Access Journals (Sweden)

    Slobodan N. Stupar

    2013-02-01

    Full Text Available Normal 0 false false false MicrosoftInternetExplorer4 This paper describes a proposal to improve the educational process of students of the Military Academy to support the maintenance process of the Serbian Army aircraft based on the introduction of objects in flight test aircraft. It is particularly emphasized the importance of establishing airline laboratories with basic characteristics of the test-measuring equipment that is necessary to integrate the aircraft to perform a practical test of an aircraft in flight. The formation of aircraft laboratories would form a very strong didactic tool, which provides for optimal synthesis of theory and practice. This concept of improving the educational process would be substantially affected the awareness of the necessity of working together and put together all the research capacity of scientific institutions in the Ministry of Defence of the Republic of Serbia.

  9. A 3D Model for Eddy Current Inspection in Aeronautics: Application to Riveted Structures

    Science.gov (United States)

    Paillard, S.; Pichenot, G.; Lambert, M.; Voillaume, H.; Dominguez, N.

    2007-03-01

    Eddy current technique is currently an operational tool used for fastener inspection which is an important issue for the maintenance of aircraft structures. The industry calls for faster, more sensitive and reliable NDT techniques for the detection and characterization of potential flaws nearby rivet. In order to reduce the development time and to optimize the design and the performances assessment of an inspection procedure, the CEA and EADS have started a collaborative work aiming at extending the modeling features of the CIVA non destructive simulation plat-form in order to handle the configuration of a layered planar structure with a rivet and an embedded flaw nearby. Therefore, an approach based on the Volume Integral Method using the Green dyadic formalism which greatly increases computation efficiency has been developed. The first step, modeling the rivet without flaw as a hole in a multi-stratified structure, has been reached and validated in several configurations with experimental data.

  10. Adapting computational optimization concepts from aeronautics to nuclear fusion reactor design

    Directory of Open Access Journals (Sweden)

    Baelmans M.

    2012-10-01

    Full Text Available Even on the most powerful supercomputers available today, computational nuclear fusion reactor divertor design is extremely CPU demanding, not least due to the large number of design variables and the hybrid micro-macro character of the flows. Therefore, automated design methods based on optimization can greatly assist current reactor design studies. Over the past decades, “adjoint methods” for shape optimization have proven their virtue in the field of aerodynamics. Applications include drag reduction for wing and wing-body configurations. Here we demonstrate that also for divertor design, these optimization methods have a large potential. Specifically, we apply the continuous adjoint method to the optimization of the divertor geometry in a 2D poloidal cross section of an axisymmetric tokamak device (as, e.g., JET and ITER, using a simplified model for the plasma edge. The design objective is to spread the target material heat load as much as possible by controlling the shape of the divertor, while maintaining the full helium ash removal capabilities of the vacuum pumping system.

  11. Infrared thermography and ultrasonics to evaluate composite materials for aeronautical applications

    Science.gov (United States)

    Boccardi, S.; Boffa, N. D.; Carlomagno, G. M.; Maio, L.; Meola, C.; Ricci, F.

    2015-11-01

    The attention of this paper is focused on the suitability of two techniques: infrared thermography and ultrasonics to evaluate impact damaged carbon/epoxy specimens. The obtained results are compared by highlighting advantages and disadvantages of each technique, as well their limits in view of an integrated use. In this context, a crucial task may be to assess the extension of delamination caused by an impact event, which may ask one to guess between sound and damaged materials at the edge of the instrument background noise. To help fixing this problem, results obtained with either lock-in thermography, or an ultrasonic phased array system, are analysed with the aid of thermographic data collected during impact tests.

  12. Quantitative impact characterization of aeronautical CFRP materials with non-destructive testing methods

    Science.gov (United States)

    Kiefel, Denis; Stoessel, Rainer; Grosse, Christian

    2015-03-01

    In recent years, an increasing number of safety-relevant structures are designed and manufactured from carbon fiber reinforced polymers (CFRP) in order to reduce weight of airplanes by taking the advantage of their specific strength into account. Non-destructive testing (NDT) methods for quantitative defect analysis of damages are liquid- or air-coupled ultrasonic testing (UT), phased array ultrasonic techniques, and active thermography (IR). The advantage of these testing methods is the applicability on large areas. However, their quantitative information is often limited on impact localization and size. In addition to these techniques, Airbus Group Innovations operates a micro x-ray computed tomography (μ-XCT) system, which was developed for CFRP characterization. It is an open system which allows different kinds of acquisition, reconstruction, and data evaluation. One main advantage of this μ-XCT system is its high resolution with 3-dimensional analysis and visualization opportunities, which enables to gain important quantitative information for composite part design and stress analysis. Within this study, different NDT methods will be compared at CFRP samples with specified artificial impact damages. The results can be used to select the most suitable NDT-method for specific application cases. Furthermore, novel evaluation and visualization methods for impact analyzes are developed and will be presented.

  13. Quantitative impact characterization of aeronautical CFRP materials with non-destructive testing methods

    Energy Technology Data Exchange (ETDEWEB)

    Kiefel, Denis, E-mail: Denis.Kiefel@airbus.com, E-mail: Rainer.Stoessel@airbus.com; Stoessel, Rainer, E-mail: Denis.Kiefel@airbus.com, E-mail: Rainer.Stoessel@airbus.com [Airbus Group Innovations, Munich (Germany); Grosse, Christian, E-mail: Grosse@tum.de [Technical University Munich (Germany)

    2015-03-31

    In recent years, an increasing number of safety-relevant structures are designed and manufactured from carbon fiber reinforced polymers (CFRP) in order to reduce weight of airplanes by taking the advantage of their specific strength into account. Non-destructive testing (NDT) methods for quantitative defect analysis of damages are liquid- or air-coupled ultrasonic testing (UT), phased array ultrasonic techniques, and active thermography (IR). The advantage of these testing methods is the applicability on large areas. However, their quantitative information is often limited on impact localization and size. In addition to these techniques, Airbus Group Innovations operates a micro x-ray computed tomography (μ-XCT) system, which was developed for CFRP characterization. It is an open system which allows different kinds of acquisition, reconstruction, and data evaluation. One main advantage of this μ-XCT system is its high resolution with 3-dimensional analysis and visualization opportunities, which enables to gain important quantitative information for composite part design and stress analysis. Within this study, different NDT methods will be compared at CFRP samples with specified artificial impact damages. The results can be used to select the most suitable NDT-method for specific application cases. Furthermore, novel evaluation and visualization methods for impact analyzes are developed and will be presented.

  14. 75 FR 28319 - Thirteenth Meeting: EUROCAE WG-72: RTCA Special Committee 216: Aeronautical Systems Security...

    Science.gov (United States)

    2010-05-20

    .... FOR FURTHER INFORMATION CONTACT: RTCA Secretariat, 1828 L Street, NW., Suite 805, Washington, DC 20036; telephone (202) 833-9339; fax (202) 833-9434; Web site http://www.rtca.org . SUPPLEMENTARY INFORMATION...:15 to 11:30: Discuss collaboration and associated topics with other organisations (Arinc, DSWG,...

  15. 77 FR 37768 - Airworthiness Directives; Aeronautical Accessories, Inc., High Landing Gear Aft Crosstube Assembly

    Science.gov (United States)

    2012-06-25

    ... R. Crane, Aviation Safety Engineer, Rotorcraft Directorate, Rotorcraft Certification Office, 2601... likely to exist or develop on other products of the same type design and that air safety and the public..., Rotorcraft Certification Office, FAA, may approve AMOCs for this AD. Send your proposal to: Martin R....

  16. Factors Affecting Innovation Within Aeronautical Systems Center (ASC) Organizations - An inductive Study

    Science.gov (United States)

    2003-03-01

    Innovation A Top Value Driver B2B 1. Innovation 2. Customer 3. Brand 4. Globalization 5. Quality B2C 1. Innovation 2. Brand 3. Customer 4. Quality...included in the appendix. The data was collected primarily via the Internet and all participants’ 18 anonymity was ensured through the use of...free to suggest new and better ways of doing things . 55.) My unit encourages appropriate risk taking. 56.) My unit challenges old ways of doing

  17. The Role of the U.S. Government Technical Report in Aeronautics: An Exploratory Study

    Science.gov (United States)

    1988-08-01

    Aeronatical STI, Technical reports, Information management, ill Accessiblifty, Information sources, Bibliometrics , Sociometrics. 16.PRICECODE 17...technologists] apply the theories and principles of science and mathematics to the economical solution of practical technical problems. 27. Type of...production, impact , and value of U.S. government technical reports.6 4 To help develop the conceptual framework for the study, studies concerned with U.S

  18. NASA and the United States educational system - Outreach programs in aeronautics, space science, and technology

    Science.gov (United States)

    Owens, Frank C.

    1990-01-01

    The role of NASA in developing a well-educated American work force is addressed. NASA educational programs aimed at precollege students are examined, including the NASA Spacemobile, Urban Community Enrichment Program, and Summer High School Apprenticeship Program. NASA workshops and programs aimed at helping teachers develop classroom curriculum materials are described. Programs aimed at college and graduate-level students are considered along with coordination efforts with other federal agencies and with corporations.

  19. Autonomic and Apoptotic, Aeronautical and Aerospace Systems, and Controlling Scientific Data Generated Therefrom

    Science.gov (United States)

    Sterritt, Roy (Inventor); Hinchey, Michael G. (Inventor)

    2015-01-01

    A self-managing system that uses autonomy and autonomicity is provided with the self-* property of autopoiesis (self-creation). In the event of an agent in the system self-destructing, autopoiesis auto-generates a replacement. A self-esteem reward scheme is also provided and can be used for autonomic agents, based on their performance and trust. Art agent with greater self-esteem may clone at a greater rate compared to the rate of an agent with lower self-esteem. A self-managing system is provided for a high volume of distributed autonomic/self-managing mobile agents, and autonomic adhesion is used to attract similar agents together or to repel dissimilar agents from an event horizon. An apoptotic system is also provided that accords an "expiry date" to data and digital objects, for example, that are available on the internet, which finds usefulness not only in general but also for controlling the loaning and use of space scientific data.

  20. Evaluating protection systems against marine corrosion of aeronautic alloy Alclad 2024-T3

    Directory of Open Access Journals (Sweden)

    William Aperador Chaparro

    2011-05-01

    Full Text Available  This paper shows how two coating systems were obtained as an alternative for protection against corrosion of al clad 2024-T3which is used in battery compartment manufacture for T-41 aircraft. Such systems consist of three types of organic resin: a first layer of P-115 polyester resin as the first coating on both systems, and a second layer of Hetron 197-3 polyester resin in the first system and vinyl-ester resin in the second one. Scanning electron microscopy (SEM was used for surface morphology analysis, showing the roughness produced by surface treatment. The coatings were electrochemically characterised by electro chemical impedance spectroscopy (EIS and Tafel polarization curves; it was found that both systems had good performance against corrosion in a marine environment and the chemical surface preparation system had a superior protective pattern for Alodine5700 + 197-3 Hetron, a 1.42x10-12mpycorrosion rate being obtained while substratum rate was 1.59x10-7 mpy. 

  1. Guidelines for developing NASA (National Aeronautics and Space Administration) ADP security risk management plans

    Science.gov (United States)

    Tompkins, F. G.

    1983-01-01

    This report presents guidance to NASA Computer security officials for developing ADP security risk management plans. The six components of the risk management process are identified and discussed. Guidance is presented on how to manage security risks that have been identified during a risk analysis performed at a data processing facility or during the security evaluation of an application system.

  2. Guidelines for development of NASA (National Aeronautics and Space Administration) computer security training programs

    Science.gov (United States)

    Tompkins, F. G.

    1983-01-01

    The report presents guidance for the NASA Computer Security Program Manager and the NASA Center Computer Security Officials as they develop training requirements and implement computer security training programs. NASA audiences are categorized based on the computer security knowledge required to accomplish identified job functions. Training requirements, in terms of training subject areas, are presented for both computer security program management personnel and computer resource providers and users. Sources of computer security training are identified.

  3. 77 FR 21404 - Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

    Science.gov (United States)

    2012-04-10

    ... the SSID. Request To Revise Compliance Time: Extend Repetitive Interval for Aft Engine Mount LM Aero...'' inspection of the aft engine mount beam (SP-190). LM Aero stated that the proposed 24-month interval would result in a significant burden on the operator to remove the aft engine mount to do the inspection....

  4. 77 FR 58210 - 31st Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data Link...

    Science.gov (United States)

    2012-09-19

    ... open to the interested public but limited to space availability. With the approval of the chairman... Meteorological Data Link Services. SUMMARY: The FAA is issuing this notice to advise the public of the thirty... review Sub-Group (SG1--Wake OSED, SG3--Architecture, SG4--DO-252 revision, SG5/6--MOPS/MAPS) status...

  5. 78 FR 20167 - 33rd Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data Link...

    Science.gov (United States)

    2013-04-03

    ... Other business ] Adjourn Attendance is open to the interested public but limited to space availability... Meteorological Data Link Services. SUMMARY: The FAA is issuing this notice to advise the public of the thirty... necessary daily EDR Turbulence Standards Project Briefing from FAA SE2020 Team SG6 WG1 Architecture...

  6. 78 FR 69928 - 35th Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data Link...

    Science.gov (United States)

    2013-11-21

    ... the interested public but limited to space availability. With the approval of the chairman, members of... Meteorological Data Link Services. SUMMARY: The FAA is issuing this notice to advise the public of the thirty... (EDR) Turbulence Project Plenary--SG3 Architecture Document FRAC Resolution 11 December...

  7. 78 FR 51808 - 34th Meeting: RTCA Special Committee 206, Aeronautical Information and Meteorological Data Link...

    Science.gov (United States)

    2013-08-21

    ... limited to space availability. With the approval of the chairman, members of the public may present oral... Meteorological Data Link Services. SUMMARY: The FAA is issuing this notice to advise the public of the thirty...: Open session on wake progress (1:00 PM) Thursday--AIS and MET Delivery Architecture...

  8. Validation and evaluation of the advanced aeronautical CFD system SAUNA: A method developer's view

    Science.gov (United States)

    Shaw, J. A.; Peace, A. J.; Georgala, J. M.; Childs, P. N.

    1993-09-01

    This paper is concerned with a detailed validation and evaluation of the SAUNA CFD system for complex aircraft configurations. The methodology of the complete system is described in brief, including its unique use of differing grid generation strategies (structured, unstructured or both) depending on the geometric complexity of the configuration. A wide range of configurations and flow conditions are chosen in the validation and evaluation exercise to demonstrate the scope of SAUNA. A detailed description of the results from the method is preceded by a discussion on the philosophy behind the strategy followed in the exercise, in terms of equality assessment and the differing roles of the code developer and the code user. It is considered that SAUNA has grown into a highly usable tool for the aircraft designer, in combining flexibility and accuracy in an efficient manner.

  9. Normal spectral emittance of Inconel 718 aeronautical alloy coated with yttria stabilized zirconia films

    Energy Technology Data Exchange (ETDEWEB)

    Gonzalez-Fernandez, L. [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Industria de Turbo Propulsores, S.A., Planta de Zamudio, Edificio 300, 48170 Zamudio, Bizkaia (Spain); Campo, L. del [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Perez-Saez, R.B., E-mail: raul.perez@ehu.es [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain); Tello, M.J. [Departamento de Fisica de la Materia Condensada, Facultad de Ciencia y Tecnologia, Universidad del Pais Vasco, Barrio Sarriena s/n, 48940 Leioa, Bizkaia (Spain)

    2012-02-05

    Highlights: Black-Right-Pointing-Pointer Emittance of Inconel 718 coated with plasma sprayed yttria stabilized zirconia. Black-Right-Pointing-Pointer The coating is opaque for {lambda} > 9 {mu}m and semi-transparent for {lambda} < 9 {mu}m. Black-Right-Pointing-Pointer In the semi-transparent region the emittance decreases with coating thickness. Black-Right-Pointing-Pointer 300 {mu}m thick coatings are still semi-transparent. Black-Right-Pointing-Pointer In the opaque region the surface roughness determines the emittance level. - Abstract: Knowledge of the radiative behaviour of the yttria stabilized zirconia (YSZ) thermal barrier coatings (TBCs) is needed to perform radiative heat transfer calculations in industrial applications. In this paper, normal spectral emittance experimental data of atmospheric plasma sprayed (PS) YSZ films layered on Inconel 718 substrates are shown. The spectral emittance was measured between 2.5 and 22 {mu}m on samples with film thicknesses ranging from 20 to 280 {mu}m. The samples were heated in a controlled environment, and the emittance was measured for several temperatures between 330 and 730 Degree-Sign C. The dependence of the spectral emittance with film thickness, surface roughness and temperature has been studied and compared with the available results for YSZ TBCs obtained by electron-beam physical vapour deposition. The PS-TBC samples show a Christiansen point at {lambda} = 12.8 {mu}m. The films are semi-transparent for {lambda} < 9 {mu}m, and opaque for {lambda} > 9 {mu}m. In the semi-transparent region, the contribution of the radiation emitted by the Inconel 718 substrate to the global emittance of the samples is analysed. In addition, the influence of the roughness in the emittance values in the opaque spectral region is discussed. Finally, the total normal emittance is obtained as a function of the TBC thickness.

  10. Aeronautical Sciences Advanced Studies Program. Delivery Order 0002: Plasma Modeling Program

    Science.gov (United States)

    2009-04-01

    A., Biagioni , L., Fantoni, G., Passaro, A., Capitelli, M., Colonna, G., Bagatin, M., and Zuin, M., Experimental investigation on the magneto...Control Devices,” AIAA Paper 2002-0350, 2002. Cristofolini, A., Borghi, C.A., Carraro, M.R., Neretti, G., Biagioni , L., Fantoni, G., and Passaro, A...Discharges,” AIAA Journal, Vol. 44, No. 7, July 2006. Forghi, C. A., Carraro, M. R., Cristofolini, A., Veefkind, A., Biagioni , L., Fantoni, G

  11. Activities involving aeronautical, space science, and technology support for minority institutions

    Science.gov (United States)

    1993-01-01

    The Final Report addressed the activities with which the Interracial Council for Business Opportunity (ICBO) was involved over the past 12 months. ICBO was involved in the design and development of a CARES Student Tracking System Software (CARES). Cares is intended to provide an effective means of maintaining relevant current and historical information on NASA-funded students through a range of educational program initiatives. ICBP was extensively involved in the formation of a minority university consortium amd implementation of collaborative research activities by the consortium as part of NASA's Mission to Planet Earth/Earth Observing System. ICBO was involved in the formation of an HBCU/MI Consortium to facilitate technology transfer efforts to the small and minority business community in their respective regions.

  12. Birth of U.S. Naval Aeronautical Engineering and Phenomenal Rise to Excellence

    Science.gov (United States)

    2011-12-01

    sea. Early work in this area consisted of adding a deck made of wood planking to existing navy ships or modifying existing...boat, and the P-3 in operation today. I . I A-l Year 1911 Wingspan 37 ft. Max Gross Weight 1,5751b Cruising Speed 51 kts Range NC-4

  13. Developing the Navy’s NC Flying Boats: Transforming Aeronautical Engineering for the First Transatlantic Flight

    Science.gov (United States)

    2011-12-01

    ft. Max Gross Weight 28,0001b Cruising Speed 84kts Range 1,278 nm Crew 6 Engines (4) 400 hp Liberty L-12 Figure 7. The NC flying boat. In...of the hull. The keel of the hull is built up from spruce while the bottom planking is laid up from two plies of cedar separated by a waterproofing...pilots could remain below decks and out of the weather if desired. The aircraft commander even had enough space to lie down on the planking that made up

  14. Boost Full Bridge Bidirectional DC/DC Converter for Supervised Aeronautical Applications

    Directory of Open Access Journals (Sweden)

    Alberto Cavallo

    2014-01-01

    Full Text Available The More Electrical Aircraft concept requires electronic devices able to efficiently and safely convert electrical power between different voltage levels. The entire realization of a bidirectional DC/DC converter, from design to validation phase, is here discussed in detail. First, a boost full bridge electrical structure is selected, adopting a Parallel Input Parallel Output (PIPO interleaving technique and an optimal turns ratio selection for the transformers in order to reduce both weight and size of the equipment. Next, modulation schemes in both step-down and step-up modes are discussed. Successively ad hoc PI regulators for both operative modes are presented. A key idea of the paper is that the converter behavior must be related not only to the control strategy but also to a global supervision logic able to safely conduct the converter operations and to react from external stimuli. Thus, a finite state machine (FSM approach is employed. An innovative strategy called buffer mode is presented, defined as an intelligent combination of buck and boost modes. Extensive simulations and experimental results are shown, in order to confirm the effectiveness of the proposed approach.

  15. 56-Day Complete Set of all of the Digital Enroute Charts - Aeronautical Information Services Digital Products

    Data.gov (United States)

    Department of Transportation — The following ZIP files contain all of the Digital Enroute charts, except for Caribbean charts, for a given effective date range. Due to the large file sizes, it is...

  16. Guidelines for contingency planning NASA (National Aeronautics and Space Administration) ADP security risk reduction decision studies

    Science.gov (United States)

    Tompkins, F. G.

    1984-01-01

    Guidance is presented to NASA Computer Security Officials for determining the acceptability or unacceptability of ADP security risks based on the technical, operational and economic feasibility of potential safeguards. The risk management process is reviewed as a specialized application of the systems approach to problem solving and information systems analysis and design. Reporting the results of the risk reduction analysis to management is considered. Report formats for the risk reduction study are provided.

  17. Aeronautical Engineering and Aerospace Engineering: A Learner-Centered Teaching Perspective in Higher Education

    Science.gov (United States)

    Gohardani, Omid; Gohardani, Amir S.; Dokter, Erin; Macario, Kyla

    2014-01-01

    Teaching in the 21st century requires a modern teaching practice coherent with the evolutions of the Information Age. Interestingly, teaching practices have stretched beyond an art form and into the realm of science. Following these scientific trails, one can argue that one of the greatest challenges educators currently face is to maintain student…

  18. 77 FR 49851 - Nineteenth Meeting: RTCA Special Committee 216, Aeronautical Systems Security (Joint Meeting With...

    Science.gov (United States)

    2012-08-17

    ... resolution of Blocking Points. Interaction with ED-201/ED-204 drafting groups, where necessary: Segregation...-202A/ED-203 09h00 to 17h00: Addressing resolution of Blocking Points. Interaction with ED-201/ED-204... Washington, DC, on August 10, 2012. David Sicard, Manager, Business Operations Branch, Federal...

  19. Refinements to Service Retention Limits for Reparable Aeronautical Components (Inactive Inventory)

    Science.gov (United States)

    2014-12-01

    E-2). Materiel managers use the ERQ algorithms incorporated into the Enterprise Resource Planning ( ERP ) to determine economic retention limits (see...of Management and Budget, Paperwork Reduction Proiect (0704-0188) Washington, DC 20503. 1. AGENCY USE O NLY (Leave blank) 12. REPORT DATE I 3. REPORT...Agency DRMS Defense Reutilization and Marketing Service ECDR expected cost to dispose or retain ERL economic retention level ERP enterprise

  20. 77 FR 63897 - Notice of License Terminations for National Aeronautics and Space Administration; Plum Brook...

    Science.gov (United States)

    2012-10-17

    ...), concerning the proposed action to decommission the NASA PBRF, appeared in the Federal Register (65 FR ] 12040... Assessment and Finding of No Significant Impact concerning this action in the Federal Register (65 FR 16421... for a Hearing'' for the PBRF in the Federal Register (72 FR 46521; August 20, 2007). On March 24,...

  1. Boeing Michigan Aeronautical Research Center (BOMARC) Missile Shelters and Bunkers Scoping Survey Report

    Science.gov (United States)

    2009-06-01

    Burley 1990), as was the case of the BOMARC WGP. PuO2 has a high melting point (2240 oC), a high chemical stability , and is highly insoluble in water...Ridge, plutonium in a holdup pond was released when a dike broke. At Rocky Flats, cutting oil contaminated with metallic plutonium was released from...factor of five. It is a moot issue for shelter 204, which was completely dismantled in 2002, and everything but the concrete floors of shelters 202

  2. 78 FR 79059 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-12-27

    ... available for review by prior appointment at the FAA Airports District Office, Mr. Richard Pur, Airports... on the Sponsor's request must be delivered or mailed to: Mr. Richard Pur, Airports Engineer, Federal... 60018. Telephone: (847) 294-7527/Fax: (847) 294-7046. FOR FURTHER INFORMATION CONTACT: Mr. Richard...

  3. 78 FR 38090 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-06-25

    .... Richard Pur, Airports Engineer, Federal Aviation Administration, Chicago Airports District Office, 2300... comments on the Sponsor's request must be delivered or mailed to: Mr. Richard Pur, Airports Engineer... Pur, Airports Engineer, Federal Aviation Administration, Chicago Airports District Office, 2300...

  4. 78 FR 36013 - Public Notice for Waiver of Aeronautical Land-Use Assurance

    Science.gov (United States)

    2013-06-14

    ... for review by prior appointment at the FAA Airports District Office, Mr. Richard Pur, Airports... comments on the Sponsor's request must be delivered or mailed to: Mr. Richard Pur, Airports Engineer... Pur, Airports Engineer, Federal Aviation Administration, Chicago Airports District Office, 2300...

  5. National Aeronautics and Space Administration Manned Spacecraft Center data base requirements study

    Science.gov (United States)

    1971-01-01

    A study was conducted to evaluate the types of data that the Manned Spacecraft Center (MSC) should automate in order to make available essential management and technical information to support MSC's various functions and missions. In addition, the software and hardware capabilities to best handle the storage and retrieval of this data were analyzed. Based on the results of this study, recommendations are presented for a unified data base that provides a cost effective solution to MSC's data automation requirements. The recommendations are projected through a time frame that includes the earth orbit space station.

  6. On the use of strain sensor technologies for strain modal analysis: Case studies in aeronautical applications

    Science.gov (United States)

    Marques dos Santos, Fábio Luis; Peeters, Bart

    2016-10-01

    This paper discusses the use of optical fiber Bragg grating (FBG) and piezo strain sensors for structural dynamic measurements. For certain industrial applications, there is an interest to use strain sensors rather than in combination with accelerometers for experimental modal analysis. Classical electrical strain gauges can be used hereto, but other types of strain sensors are an interesting alternative with some very specific advantages. This work gives an overview of two types of dynamic strain sensors, applied to two industrial applications (a helicopter main rotor blade and an F-16 aircraft), FBG sensors and dynamic piezo strain sensors, discussing their use and benefits. Moreover, the concept of strain modal analysis is introduced and it is shown how it can be beneficial to apply strain measurements to experimental modal analysis. Finally, experimental results for the two applications are shown, with an experimental modal analysis carried out on the helicopter main rotor blade using FBG sensors and a similar experiment is done with the aircraft but using piezo strain sensors instead.

  7. Validation of Alternatives to High Volatile Organic Compound Solvents Used in Aeronautical Antifriction Bearing Cleaning

    Science.gov (United States)

    2006-10-17

    Rinse – Step 3 Fluid Agitated Tank MIL-PRF-680 (Filtered –10 μ) 5 min. 8 Dry Isopropyl Alcohol Dryer Isopropyl Alcohol As Required 9 Inspection None...Isopropyl Alcohol Dryer 8 Dry Isopropyl Alcohol As Required 9 Inspection None None As Required Neutralize Fingerprints 10 Fluid Agitated Tank...control regulations for effect on the design and operation of pressurized solvent spray equipment. h. Vibro- Tumbling Finishing Mills. Several

  8. Experimental Study of the Induced Residual Stresses During the Manufacturing Process of an Aeronautic Composite Material

    Directory of Open Access Journals (Sweden)

    Hussam Kassem

    2010-09-01

    Full Text Available A methodology is proposed for predicting the formation and the development of the manufacturing residual stresses, this approach is based on the study of the evolution of the resin yield stress. In order to evaluate our method, a comparison has been made between the yield time (corresponding to the formation of a yield stress and the gel time. A self-consistent model is used to determine the cure-dependent chemical shrinkage coefficient of the composite material. This model allows considering for the composite material behavior an anisotropic chemical shrinkage, which is not represented by a classical linear model. An experimental approach based on the peel-ply method is used to determine the distribution of the residual stresses through the thickness.

  9. Creation of an Aeronautical Capstone Design Project Program at Ohio State University

    Science.gov (United States)

    2014-12-08

    personnel recovery operations. The Air Force Pararescuers (PJs) are skilled in treating injuries and bringing 6 people out of difficult situations day...each other and may be packed into the rucksack. The disassembly time using this method with four people is ____. FIGURE through FIGURE show the...the goal was to “keep it simple, stupid ” and produce a tool designed for the airmen and their specific needs. To ensure the ergonomics of the device

  10. Evaluation of Defects in Multilayer Carbon Fibre Epoxy for Aeronautics Applications

    Directory of Open Access Journals (Sweden)

    M. Buonsanti

    2009-01-01

    Full Text Available Production of carbon fibre reinforced polymers is an elaborate process unfree from faults and problems. Problems during the manufacturing, such as plies' overlapping, can cause flaws in the resulting material, so compromising its integrity. Compared with metallic materials, carbon epoxy composites show a number of advantages. Within this framework, ultrasonic tests are effective to identify the presence of defects. In this paper a Finite Element Method approach is proposed for evaluating the most effective incidence angle of an ultrasonic probe with regard to defects' identification. According to our goal, the analysis has been carried out considering a single-line plane emitting source varying the probe angle of inclination. The proposed model looks promising to specially emphasize the presence of delaminations as well as massive breaking in a specimen of multilayer carbon fibre epoxy. Subsequently, simulation parameters and results have been exploited and compared, respectively, for a preliminary experimental in-lab campaign of measurements with encouraging results.

  11. Michigan/Air Force Research Laboratory (AFRL) Collaborative Center in Aeronautical Sciences (MACCAS)

    Science.gov (United States)

    2013-09-01

    temperature (which were recorded and are available one the website), PIV micron sized oil drops lagging behind the flow variations near the shock wave, and...However, for external flows, the conductivity should drop to a negligible value far from the body such that it is assumed permissible to set the normal...usually evaluated as: v = MW + P (3) with the first term due to Millikan and White [2] and the second term, a high temperature

  12. A Review of Australian Investigations on Aeronautical Fatigue During the Period April 1983 to March 1985.

    Science.gov (United States)

    1985-03-01

    Quantitiative NDE, La Jolla, California, 1984. S... 9/46 59. Scala, C.M. and Cousland, S.NcK. Acoustic emission from the aluminium alloy 6061 -T651. J. Mats...replaces the original aluminium component. To ensure the continued airworthiness of aluminium brackets still in service, the manufacturer has conducted...characteristics of an aluminium alloy is being expanded incrementally up to 5% of diameter. Incremental unloading will follow. Subsequently, the

  13. Implementation of Electronic Commerce in the Department of Defense and the National Aeronautics and Space Administration.

    Science.gov (United States)

    1996-12-01

    President Clinton’s Executive Memorandum of 26 October 1993 mandated that all Federal Government agencies implement Electronic Commerce (EC) in order... Electronic Commerce /Electronic Data Interchange (EC/EDI) architecture. The NASA employed an Internet based tool, the NASA Acquisition Internet Service

  14. 77 FR 33254 - Expediting Transition of Government Performed and Sponsored Aeronautics Research and Development

    Science.gov (United States)

    2012-06-05

    ... economic growth, the creation of high-quality jobs, and national security. In addition, as a means to... strategies of non-Federal stakeholders. DATES: Comments will be received through July 16, 2012, 11:59 p.m.... Any proprietary or business confidential information that is submitted in response to this...

  15. Detection of drilling-induced delamination in aeronautical composites by noncontact laser ultrasonic method.

    Science.gov (United States)

    Zhou, Zhenggan; Sun, Guangkai; Chen, Xiucheng; Wang, Jie

    2014-04-20

    A novel application of the laser ultrasonic technique for the detection of drilling-induced delamination in composite components of aircrafts is proposed. Numerous key components of aircrafts are made of composite materials, and drilling is often a final operation during assembly. Drilling-induced delamination significantly reduces the structural reliability, and it is rather difficult to be detected effectively and automatically. The laser ultrasonic technique is a promising method to solve the problem. This paper investigates the characterization of drilling-induced delamination in composites by a noncontact laser ultrasonic method. A carbon fiber reinforced plastic laminate with drilling holes is prepared as a specimen. The characterization of drilling-induced delamination with laser-generated ultrasonic waves is investigated theoretically and experimentally, and the morphology features of the delamination are obtained by laser ultrasonic C-scan testing. The results prove that the laser ultrasonic technique is effective for the detection of drilling-induced delamination in composite components, and it is a feasible solution for evaluating the drilling quality during assembly.

  16. Technologic Papers of the Bureau of Standards. Number 237. Aeronautic Instruments,

    Science.gov (United States)

    2007-11-02

    the motion of the airplane or on the speed of rotation of small cup anemometers ’or air propellers. -The indicati6ns of the pressure type are pro...developed by these instruments also obeys the pv2 law. In instruments of the anemometer type the air speed is determined by the rate of revolution by a cup ...to a third sighting Huntl Aeronautitc In struments. 461 FIG. 13.-Pensuti pressure plate air-speed indicator. FIG. 14.-Morell cup anemometer air-speed

  17. Application of Carbon Based Nano-Materials to Aeronautics and Space Lubrication

    Science.gov (United States)

    Street, Kenneth W., Jr.; Miyoshi, Kazuhisa; Wal, Randy L. Vander

    2007-01-01

    The tribology program at NASA Glenn Research Center in Cleveland, Ohio, is investigating carbon based nano-particles for their potential in advanced concept lubrication products. Service conditions range from high temperature atmospheric to low temperature vacuum. Some of the lubricants and surface coatings of tribological significance that we have evaluated include neat nano-particles, both grown in-situ and as bulk material deposited on the substrate, and nano-particles dispersed in oils which are all highly substrate interactive. We discuss results of testing these systems in a spiral orbit tribometer (SOT) and a unidirectional pin-on-disc (PoD) tribometer. A nano-onions/Krytox mixture evaluated as a lubricant for angular contact bearings in air caused a marked lowering of the coefficient of friction (CoF) (0.04 to 0.05) for the mixture with an eight-fold improvement in lifetime over that of the Krytox alone. In vacuum, no effect was observed from the nano-onions. Multi-walled nanotubes (MWNT) and graphitized MWNT were tested under sliding friction in both air and vacuum. The MWNT which were grown in-situ oriented normal to the sliding surface exhibited low CoF (0.04) and long wear lives. Bulk MWNT also generate low CoF (0.01 to 0.04, vacuum; and 0.06, air) and long wear life (>1 million orbits, vacuum; and >3.5 million, air). Dispersed graphitized MWNT were superior to MWNT and both were superior to aligned MWNT indicating that orientation is not an issue for solid lubrication. Single-walled nanotubes (SWNT) were modified by cutting into shorter segments and by fluorination. All SWNTs exhibited low CoF in air, with good wear lives. The SWNT with slight fluorination yielded an ultra-low CoF of 0.002 although the best wear life was attributed to the nascent SWNT.

  18. Proposal for the Conceptual Design of Aeronautical Final Assembly Lines Based on the Industrial Digital Mock-Up Concept

    OpenAIRE

    Mas Morate, Fernando; Gómez, Alejandro; Menéndez Cuñado, José Luis; Ríos Chueco, José

    2013-01-01

    Part 1: Keynotes; International audience; The design of a Final Assembly Line (FAL) is carry out in the product industrialization activity. The phase dealing with the definition of conceptual solutions is characterized by depending heavily on the personnel experience and being time-consuming. To enhance such process, it is proposed a development of a knowledge based software application to assist designers in the definition of scenarios and to generate conceptual FAL alternatives. Both the sc...

  19. Prediction of Foreign Object Debris/Damage type based in human factors for aeronautics using logistic regression model

    Science.gov (United States)

    Romo, David Ricardo

    Foreign Object Debris/Damage (FOD) has been an issue for military and commercial aircraft manufacturers since the early ages of aviation and aerospace. Currently, aerospace is growing rapidly and the chances of FOD presence are growing as well. One of the principal causes in manufacturing is the human error. The cost associated with human error in commercial and military aircrafts is approximately accountable for 4 billion dollars per year. This problem is currently addressed with prevention programs, elimination techniques, and designation of FOD areas, controlled access, restrictions of personal items entering designated areas, tool accountability, and the use of technology such as Radio Frequency Identification (RFID) tags, etc. All of the efforts mentioned before, have not show a significant occurrence reduction in terms of manufacturing processes. On the contrary, a repetitive path of occurrence is present, and the cost associated has not declined in a significant manner. In order to address the problem, this thesis proposes a new approach using statistical analysis. The effort of this thesis is to create a predictive model using historical categorical data from an aircraft manufacturer only focusing in human error causes. The use of contingency tables, natural logarithm of the odds and probability transformation is used in order to provide the predicted probabilities of each aircraft. A case of study is shown in this thesis in order to show the applied methodology. As a result, this approach is able to predict the possible outcomes of FOD by the workstation/area needed, and monthly predictions per workstation. This thesis is intended to be the starting point of statistical data analysis regarding FOD in human factors. The purpose of this thesis is to identify the areas where human error is the primary cause of FOD occurrence in order to design and implement accurate solutions. The advantages of the proposed methodology can go from the reduction of cost production, quality issues, repair cost, and assembly process time. Finally, a more reliable process is achieved, and the proposed methodology may be used in other aircrafts.

  20. [Importance, especially in aeronautics, of color perception tests under dynamic conditions. Study of a suitable experimental apparatus].

    Science.gov (United States)

    Linzi, S; Modugno, G C; Bollini, M

    1977-12-15

    Following a review of the most recent opinion on the physiology of colour vision, a device for examining it in dynamic, i.e. real-life conditions is described. The apparatus consist of two projectors which flash two absolutely identical pictures on to the screen, one of them is upside down. It appears at fixed but adjustable intervals so that the exposure time of the intelligible image can be varied. Subjects were also controlled with Ishihara charts and Nägel anomaloscope. The results are compared and point to the higher sensitivity of the dynamic test to even slight degrees of dyschromatopsia.

  1. Modeling, fabrication and plasma actuator coupling of flexible pressure sensors for flow separation detection and control in aeronautical applications

    Science.gov (United States)

    Francioso, L.; De Pascali, C.; Pescini, E.; De Giorgi, M. G.; Siciliano, P.

    2016-06-01

    Preventing the flow separation could enhance the performance of propulsion systems and future civil aircraft. To this end, a fast detection of boundary layer separation is mandatory for a sustainable and successful application of active flow control devices, such as plasma actuators. The present work reports on the design, fabrication and functional tests of low-cost capacitive pressure sensors coupled with dielectric barrier discharge (DBD) plasma actuators to detect and then control flow separation. Finite element method (FEM) simulations were used to obtain information on the deflection and the stress distribution in different-shaped floating membranes. The sensor sensitivity as a function of the pressure load was also calculated by experimental tests. The results of the calibration of different capacitive pressure sensors are reported in this work, together with functional tests in a wind tunnel equipped with a curved wall plate on which a DBD plasma actuator was mounted to control the flow separation. The flow behavior was experimentally investigated by particle image velocimetry (PIV) measurements. Statistical and spectral analysis, applied to the output signals of the pressure sensor placed downstream of the profile leading edge, demonstrated that the sensor is able to discriminate different ionic wind velocity and turbulence conditions. The sensor sensitivity in the 0-100 Pa range was experimentally measured and it ranged between 0.0030 and 0.0046 pF Pa-1 for the best devices.

  2. 77 FR 61047 - Public Notice for Waiver of Aeronautical Land-Use Assurance: Bolton Field Airport; Columbus, OH

    Science.gov (United States)

    2012-10-05

    ... Storage Systems, LLC by deed of record in Instrument Number 200512090260149; Thence North 02 02'58'' East... 200211250301573, the Second Amendment to The Villas at Holt Run Condominium, Instrument Number 200807220112257... Run Condominium, Instrument Number 200212030308781, the line common to Holt Run, a subdivision...

  3. The National Aeronautics and Space Administration-U.S. Public Health Service Health Evaluation and Enhancement Program - Summary of results.

    Science.gov (United States)

    Durbeck, D. C.; Heinzelmann, F.; Schacter, J.; Haskell, W. L.; Payne, G. H.; Moxley, R. T., III; Nemiroff, M.; Limoncelli, D. D.; Arnoldi, L. B.; Fox, S. M., III

    1972-01-01

    An exercise program was initiated in a federal agency to assess the feasibility of such a program, and to identify the factors that influenced joining, adherence to, and effectiveness of the program. The program was utilized by 237 of the 998 eligible federal employees; mean attendance rate was 1.3 days/week. Those who volunteered perceived a need for increased physical activity, believed they had sufficient time to participate and derived subjective as well as objective benefits. Significant improvements were found in heart rate response to the standard exercise test, body weight, skinfold measurements and triglyceride levels.

  4. 14 CFR 61.313 - What aeronautical experience must I have to apply for a sport pilot certificate?

    Science.gov (United States)

    2010-01-01

    ...-control aircraft category land or sea class privileges, (1) 20 hours of light time, including 15 hours of flight training from an authorized instructor in a weight-shift-control aircraft and at least 5 hours...

  5. 14 CFR 61.411 - What aeronautical experience must I have to apply for a flight instructor certificate with a...

    Science.gov (United States)

    2010-01-01

    ...-shift-control aircraft category privileges, (1) 150 hours of flight time as a pilot, (i) 100 hours of...-control aircraft, (iii) 25 hours of cross-country flight time, (iv) 10 hours of cross-country flight time in a weight-shift-control aircraft, and (v) 15 hours of flight time as pilot in command in a...

  6. 76 FR 82035 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Ohio State University Airport...

    Science.gov (United States)

    2011-12-29

    ... North, Range 19 West, United States Military District, being part of the 49.198 acre tract conveyed to... 49' 22'' West for the centerline of Dublin-Granville Road, as established by a GPS network of...

  7. 76 FR 25402 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Richard Downing Airport, Coshocton, OH

    Science.gov (United States)

    2011-05-04

    ... Ohio, and being further described as follows; Note: North based on GPS observations. All steel pins... Township 6 North, Range 6 West, United States Military Lands, in Township of Keene, in the County...

  8. Postdoctoral and Senior Postdoctoral Resident Research Associateship Program and Research Management Associateship Program for the National Aeronautics and Space Administration

    Science.gov (United States)

    1986-01-01

    Information on the status of all Resident Research Associated and Research Management Associates is provided. All Associated whose tenure continued as of June 1, 1985 are listed alphabetically by laboratory. Also included are their countries of citizenship and dates of tenure. The status of reporting obligations are summarized. A list of progress reports received during this reporting period is also provided. All Associates who terminated during the reporting period are listed.

  9. Summary Report of the NASA Management Study Group: Recommendations to the Administrator, National Aeronautics and Space Administration

    Science.gov (United States)

    Phillips, Samuel C.

    1986-01-01

    The NASA Management Study Group (NMSG) was established under the auspices of the National Acedamy of Public Administration at the request of the Administrator of NASA to assess NASA's management practices and to evaluate the effectiveness of the NASA organization. This report summarizes the conclusions and recommendations of the NMSG on the overall management and organization of NASA.

  10. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1998. Volume 1

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Sickorez, Donn G. (Editor)

    1999-01-01

    JSC NASA/ASEE Summer Faculty Fellowship Program was conducted by the University of Houston and JSC, under ASEE. The objectives of the program are to further the professional knowledge of qualified engineering and science members; stimulate an exchange of ideas between participants and NASA; enrich and refresh the research and teaching activities of participants; and contribute to the research objectives of the NASA Centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project commensurate with his/her interests and background and worked in collaboration with a NASA/JSC colleague. This document is a compilation of the final reports on the fellows' research projects performed during the summer of 1998. Volume 1, current volume, contains the first reports, and volume 2 contains the remaining reports.

  11. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program: 1996. Volume 2

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Sickorez, Donn G. (Editor)

    1997-01-01

    The objectives of the program, which began nationally in 1964 and at JSC in 1965 are to (1) further the professional knowledge qualified engineering and science faculty members, (2) stimulate an exchange of ideas between participants and NASA, (3) and refresh the research and teaching activities of participants' institutions, and (4) contribute to the research objectives of NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA JSC colleague.

  12. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program: 1995.. Volume 2

    Science.gov (United States)

    Hyman, William A. (Editor); Sickorez, Donn G. (Editor)

    1996-01-01

    The JSC NASA/ASEE Summer Faculty Fellowship Program was conducted at JSC, including the White Sands Test Facility, by Texas A&M University and JSC. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of the participants' institutions; and (4) to contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA/JSC colleague. In addition to the faculty participants, the 1995 program included five students. This document is a compilation of the final reports on the research projects completed by the faculty fellows and visiting students during the summer of 1995. The reports of two of the students are integral with that of the respective fellow. Three students wrote separate reports.

  13. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program: 1995. Volume 1

    Science.gov (United States)

    Hyman, William A. (Editor); Sickorez, Donn G. (Editor)

    1996-01-01

    The objectives of the JSC NASA/ASEE Summer Faculty Fellowship Program, which began nationally in 1964 and at JSC in 1965, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of the participants' institutions; and (4) to contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA/JSC colleague. In addition to the faculty participants, the 1995 program included five students. This document is a compilation of the first fifteen of twenty-seven final reports on the research projects completed by the faculty fellows and visiting students during the summer of 1995. The reports of two of the students are integral with that of the respective fellow. Three students wrote separate reports included in Volume 2.

  14. National Aeronautics and Space Administration (NASA) /American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program. Volume 1

    Science.gov (United States)

    Bannerot, Richard B. (Editor); Sickorez, Donn G. (Editor)

    1997-01-01

    The 1996 JSC NASA/ASEE Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The objectives of the program, which began nationally in 1964 and at JSC in 1965 are to (1) further the professional knowledge qualified engineering and science faculty members, (2) stimulate an exchange of ideas between participants and NASA, (3) refresh the research and teaching activities of participants' institutions, and (4) contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA JSC colleague. This document is a compilation of the final reports on the research projects completed by the faculty fellows during the summer of 1996.

  15. The National Aeronautics and Space Administration’s FY2006 Budget Request: Description, Analysis, and Issues for Congress

    Science.gov (United States)

    2006-01-24

    displays, gauges, and instruments • First flight test of winglets (small wings at the end of each main wing) to reduce aerodynamic drag, improving fuel...technologies such as composite airframe materials, but program cancelled in 1994. 1990-1999 • Continued flights of the Space Shuttle: - 64 successful

  16. 77 FR 49479 - Public Notice for Waiver Of Aeronautical Land-Use Assurance; Springfield-Beckley Municipal...

    Science.gov (United States)

    2012-08-16

    ... for CLA-794-0.60, of record in Plat Book 18, page 286, and said parcel being further bounded and... centerline of construction for State Route 794, as shown on the centerline plat for CLA-794-0.60, of record... 794, both as shown on the centerline plat for CLA-794- 0.60, of record in Plat Book 18, page 286,...

  17. A CDMA Spotbeam Architecture for the Next Generation Satellite System (NGSS) for the Aeronautical Telecommunications Network (ATN)

    Science.gov (United States)

    Raghavan, Rajesh S.; Shamma, Mohammed A.

    2003-01-01

    This paper will present work being done to model and simulate a CDMA based Mobile Satellite System architecture for providing all or part of the future Air Traffic Management (ATM) services. Such a system, will help in relieving the dependence on ground based networks, if not eliminate it. Additionally such an architecture can be used in parallel or as a supplementary service along with ground based links to help alleviate any capacity bottlenecks, or in areas where such services are difficult to make available such as in oceanic, remote areas outside the jet highways, or in developing countries where ground services are less available.

  18. A Study of the Attitudes of Acquisition Managers and Engineers at Aeronautical Systems Division and Space Systems Division

    Science.gov (United States)

    1989-09-01

    Frederick Herzberg in the way employees are motivated. Herzberg divided the factors which were intrinsic to the job itself into two categories. The... Herzberg contended that the real way to motivate employees was to focus on the motivation factors in the iob itself. Most management policies at the

  19. Calendar of Selected Aeronautical and Space Meetings January 1988 (Calendrier des Manifestations Aeronautiques et Spatiales (Selection) Janvier 1988).

    Science.gov (United States)

    1987-12-01

    iti(Ilics. dCI.. Bien toii iitIi, )il ol tic \\Lcritici LI c vrccii dc ti sntorni11itu’ ins ticuvl~ail thins cowt brliniuc .VI AC.Ri ) Ile pcui Ci1 IO...Salons et Expositions 87 1 2 C-ours de formation 90 *\\Jeuiilei noter que la rubrique 10 doit etre consulte en plus de celles de 0 1 09O. 4-’- 0- ~Lr -J e

  20. 77 FR 60167 - Public Notice For Waiver of Aeronautical Land-Use Assurance; Former Willmar Municipal Airport...

    Science.gov (United States)

    2012-10-02

    ... distance of 321.10 feet, along a curve, which is concave to the east, having a radius of 11359.16 feet, a... a proposal to authorize the release of 138.33 acres of airport property at the former Willmar Municipal Airport, Willmar, MN. The land will be used for an industrial park. The FAA issued a ]...

  1. 77 FR 24253 - Public Notice for Waiver of Aeronautical Land-Use Assurance Former Willmar Municipal Airport...

    Science.gov (United States)

    2012-04-23

    ... 103.01 feet, along a curve, which is concave to the east, having a radius of 11359.16 feet, a central...; Thence northerly, a distance of 118.08 feet, along a curve, which is concave to the east, having a radius..., having a radius of 150.00 feet, a central angle of 36 degrees 24 minutes 52 seconds, and a......

  2. Publications of the Division of Mechanical Engineering and the National Aeronautical Establishment. Series Number 2, Supplement Number 7.

    Science.gov (United States)

    1982-01-01

    1219 A Survey of Fatal Aircraft Accidents Involving Metal Fatigue - Final Report, by G.S. Campbell, December 1980. LTR-ST-1224 Le Choix des Materiaux ...Cutting Cold River Ice with Water Jets during the Winter 1977-78, by D.B. Coveney and W.H. Brierley, June 1979. LTR-LT-100 Traction Motor Suspension ...and P.F. Hearty, November 1979. LTR-LT-106 Traction Motor Suspension Bearing Leakage Tests. Phase 11, by J.F. Lane and D.E. Morris, October 1979. LTR-LT

  3. 75 FR 54418 - Public Notice for a Change in Use of Aeronautical Property Associated With Wiscasset Municipal...

    Science.gov (United States)

    2010-09-07

    ... to George L. Worden it ux, dated May 29, 1968 and recorded in the Lincoln County Registry of Deeds... August 25, 2010. LaVerne F. Reid, Manager, Airports Division, New England Region. BILLING CODE 4910-13-M...

  4. 76 FR 74844 - Public Notice for Waiver of Aeronautical Land-Use Assurance at Auburn-Lewiston Municipal Airport...

    Science.gov (United States)

    2011-12-01

    ... Investment and Reform Act for the 21st Century (AIR 21) requires the FAA to provide an opportunity for public... northwesterly line of said McLeod 435.53' to a 5 rebar with cap stamped ``NCS, INC PLS 1314'' set in the... and land N/F of City of Auburn and City of Lewiston (Airport Property) 200.49' to a 5 rebar with...

  5. Calendar of Selected Aeronautical and Space Meetings (Calendrier des Manifestations Aeronautiques et Spatiales (Selection). Juillet-July 1984.

    Science.gov (United States)

    1984-06-01

    PAYS AR Argentina JA Japan AU Austria LU Luxenbourg BE Belgium ME Mexico BR Brazil MO Monaco BU Bulgaria NL Netherlands CA Canada NO Norway CH...Ulbures and Information Bureaux: 3 Belgrave Square, London, SWIX 8PL UK ASM American Society for Metals: Metals Park, OH 44073 US ASMA Aemace Medical

  6. Calendar of Selected Aeronautical and Space Meetings July 1988 (Calendrier des Manifestations Aeronautiques et Spatiales (Selecgion) Juillet 1988)

    Science.gov (United States)

    1988-07-01

    Argentina IT Italy AU Austria JA Japan BA Bermuda KE Kenya BE Belgium LU Luxembourg BR Brazil ME Mexico BU Bulgaria MO Monaco CA Canada NL Netherlands...Tel. (216) 338-5151 US ASMA Aerospace Medical Association: National Airport, Washington, DC 20001-4977. Tel. (703) 892-2240 US ASME American Society...AL 36109- US ISNPS Institute for Spame Nuclear Power Studies: Chemical and Nuclear Engineering Dept., University of New Mexico , Albuquerque, NM 87131

  7. Calendar of Selected Aeronautical and Space Meetings July 1987 (Calendrier des Manifestations Aeronautiques et Spatiales (Selection) Juillet 1987).

    Science.gov (United States)

    1987-07-01

    CODE CODE DES PAYS AR Argentina JA Japan AU Austria KE Kenya BF Belgium LU Luxembourg BR Brazil ME Mexico BI Bulgana MO Monaco (A Canada NL...Information Management : 26-27 Boswell Street, London. WCIN 3JZ UK ASM American Society for Metals: Metals Park, OH 44073 US ASMA Aerospace Medical

  8. Calendar of Selected Aeronautical and Space Meetings December 1985 (Calendrier des Manifestations Aeronautiques et Spatiales (Selection) Decembre 1985).

    Science.gov (United States)

    1985-12-01

    CODE CODE DES PAYS AR Argentina JA Japan AU Austria LU Luxembourg BE Belgium ME Mexico BR Brazil MO Monaco BU Bulgaria NL Netherlands CA Canada NO...for Metals: Metals Park, OH 44073 US ASMA Aerospace Medical Association: National Airport, Washington, DC 20001 - 4977 US ASM F American Society of

  9. [Production technology and use of composite materials in the aeronautics industry, risks and pathology in the manufacturing workers].

    Science.gov (United States)

    Franco, G; Candura, F

    1985-01-01

    The type and applications of composite materials have increased greatly during the last forty years, particularly in the aircraft and aerospace industries. The foreseeable increase of the employment of composite materials in future needs an adequate engagement in finding out health risks involved with technological processes. Composite materials - considered as a close union between a continuous glass, aramid or carbon reinforcing fibre and a epoxy matrix - present several advantages over traditional materials. Structural epoxy adhesives are defined as complex formulated systems. By mixing a large number of ingredients a formulated resin is obtained, which represents the start of the production process for adhesive manufacture. The most important ingredients such as catalysts, accelerators, the groups of epoxy monomers and oligomers, additives most used and their role into the epoxy matrices are illustrated. Of the various technologies existing for the fabrication of aircraft structures the one so called "vacuum bag" is described. The knowledge of the chemical composition of the substances used in the production of composite materials and epoxy adhesives allows to verify the possible existence of hazard for workers health. Among the potentially dangerous chemicals, epoxy monomers and oligomers, catalysts, accelerators are to be considered. The metabolism and the mechanisms of toxicity of epoxides are summarized. However the toxic effects of most epoxides are far from being wholly investigated. In man epoxides ingestion, inhalation or absorption through the skin can lead to several toxic effects: irritation and sensitisation, alterations of liver and nervous function. Finally some epoxides are considered to be carcinogenic in animals and in man; however for many compounds, the results are not yet conclusive. From what it is said above come out the necessity of a careful sanitary control of the workers exposed to these hazards, control that is made difficult by the lack of adequate biological indices for the risks found.

  10. Hearings Before the Committee on Aeronautical and Space Sciences. United States Senate, Ninety-Third Congress, Second Session

    Science.gov (United States)

    1974-07-18

    low turbines and the second low turbine as in a straight turbojet, and (b) the front fan and then through an auxiliary nozzle similar to the operation...passing through the second low tur- bine, and (b) the duct heater and the rear flow diverter valve to power the second low turbine . In the supersonic...cruise mode, the engine is in essence a dual turbojet with the intake airflow matched to the requirements of the com- pressor/burner/high and low turbine path

  11. A Review of Australian and New Zealand Investigations on Aeronautical Fatigue During the Period April 2007 to March 2009

    Science.gov (United States)

    2009-04-01

    least 2,500 hours. 1. 361-WEB-5, OW Lwr front spar web @ WS216 381-PDN-2, OW Lwr pnl #1 DNH-Fairing Fillet @ WS335 485-CUT-1, OW Up pnl #3 door cutout... pnl splice DNH @ WS218 2. 3. 4. 5. 6. Figure 11 RAAF P-3C Orion IAT Tracking Locations 8-17 DSTO-TN-0885 SDRS 5 WS76 SDRS 6 WS147 SDRS 7

  12. Dynamic Strain Measurements on Automotive and Aeronautic Composite Components by Means of Embedded Fiber Bragg Grating Sensors

    OpenAIRE

    Alfredo Lamberti; Gabriele Chiesura; Geert Luyckx; Joris Degrieck; Markus Kaufmann; Steve Vanlanduit

    2015-01-01

    The measurement of the internal deformations occurring in real-life composite components is a very challenging task, especially for those components that are rather difficult to access. Optical fiber sensors can overcome such a problem, since they can be embedded in the composite materials and serve as in situ sensors. In this article, embedded optical fiber Bragg grating (FBG) sensors are used to analyze the vibration characteristics of two real-life composite components. The first component...

  13. Man-Machine Integration Design and Analysis System (MIDAS) v5: Augmentations, Motivations, and Directions for Aeronautics Applications

    Science.gov (United States)

    Gore, Brian F.

    2011-01-01

    As automation and advanced technologies are introduced into transport systems ranging from the Next Generation Air Transportation System termed NextGen, to the advanced surface transportation systems as exemplified by the Intelligent Transportations Systems, to future systems designed for space exploration, there is an increased need to validly predict how the future systems will be vulnerable to error given the demands imposed by the assistive technologies. One formalized approach to study the impact of assistive technologies on the human operator in a safe and non-obtrusive manner is through the use of human performance models (HPMs). HPMs play an integral role when complex human-system designs are proposed, developed, and tested. One HPM tool termed the Man-machine Integration Design and Analysis System (MIDAS) is a NASA Ames Research Center HPM software tool that has been applied to predict human-system performance in various domains since 1986. MIDAS is a dynamic, integrated HPM and simulation environment that facilitates the design, visualization, and computational evaluation of complex man-machine system concepts in simulated operational environments. The paper will discuss a range of aviation specific applications including an approach used to model human error for NASA s Aviation Safety Program, and what-if analyses to evaluate flight deck technologies for NextGen operations. This chapter will culminate by raising two challenges for the field of predictive HPMs for complex human-system designs that evaluate assistive technologies: that of (1) model transparency and (2) model validation.

  14. Neurospora experiment P-1037. Quarterly progress report to the National Aeronautics and Space Administration, October 1--December 15, 1966

    Energy Technology Data Exchange (ETDEWEB)

    1967-12-01

    The main values of the 302 gantry exercise were to check the preparation of the Neurospora experiment and the spacecraft loading procedure under timed conditions and to provide final assurance that necessary operations can be completed with appropriate inspection in the allotted time. Because of the brief time interval between the 302 Gantry Exercise and the scheduled Biosatellite A flight, no attempt was made to assay for forward-mutation frequecies; however, biocompatibility tests were performed on the 302 hardware by plating conidia from a number of the modules in the usual fashion to assay survival. The average heteokaryotic conidial survival was 82.6%, which is sufficiently high for use of the conidia in a forward-mutation experiment. Calibration of thermoluminescent dosimeters was carried out using a /sup 85/Sr ..gamma.. source.

  15. Approaches to S&T Cost Modeling at the U.S. Air Force Research Laboratory/Vehicle Aeronautics Directorate

    Science.gov (United States)

    2000-09-01

    Manufacturing Operation Sequence 4-1 Une expe~rience de I’inge~ni e-rie concourante de navires de guerre et de leur soutien logistique Jean-Philippe...utilisateurs, les technologies mises en ceuvre (y exhaustives. Le soutien logistique intdgr6 et la compris celles de la conception), le monde...et abandonner le concept " touj ours pr&t A tout partout A tout moment " au profit d’un miveau de risque raisonnable ; 3.1. Le soutien logistique int

  16. Status of Department of Defense Architecture Framework (DoDAF) Implementation within the Aeronautical Systems Center (ASC)

    Science.gov (United States)

    2007-11-02

    characterizes these complex, unprecedented systems” (26:6). Further, Howard Eisner offers the following in his book, Essentials of Project and Systems...definitions deal with architectures role in the design of the system. Howard Eisner, author of Essentials of Project and Systems Engineering Management...prescribed several views as beneficial to the program manager in acquisition strategy development. Further, as Zinn noted, with the Clinger-Cohen Act

  17. 航空树脂基复合材料技术发展%Aeronautical Polymer Matrix Composites' Technological Development

    Institute of Scientific and Technical Information of China (English)

    盛永清

    2008-01-01

    通过介绍我国航空树脂基复合材料的发展现状和应用情况,讨论并分析了航空树脂基复合材料未来的发展趋势和重点方向,强调了这种"低成本"、"工程化"技术应在"一体化"思想指导下综合协调发展.

  18. 77 FR 7656 - Public Notice for Waiver for Aeronautical Land-Use Assurance at Will Rogers World Airport...

    Science.gov (United States)

    2012-02-13

    ... conversion of these parcels will benefit the aviation community by reinvestment in the airport. Approval does... property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition...

  19. Government Information Quarterly. Volume 7, no. 2: National Aeronautics and Space Administration Scientific and Technical Information Programs. Special issue

    Science.gov (United States)

    Hernon, Peter (Editor); Mcclure, Charles R. (Editor); Pinelli, Thomas E. (Editor)

    1990-01-01

    NASA scientific and technical information (STI) programs are discussed. Topics include management of information in a research and development agency, the new space and Earth science information systems at NASA's archive, scientific and technical information management, and technology transfer of NASA aerospace technology to other industries.

  20. An Update of the Nation’s Long-Term Strategic Needs for NASA’s Aeronautics Test Facilities

    Science.gov (United States)

    2009-01-01

    Ames Crew- Vehicle Systems Research Facility (CVSRF) • Possible use for DDT&E and crew training • Motion cues to assess manual control capability...Flight Deck: generic glass cockpit – Research Flight Deck: hybrid B-777/MD-11/ A320 – Integration Flight Deck: modified B-757 (Source: NASA Langley) NASA

  1. Wright Brothers Lectureship in Aeronautics: Experience with HiMAT remotely piloted research vehicle - An alternate flight test approach

    Science.gov (United States)

    Deets, D. A.; Brown, L. E.

    1986-01-01

    The highly maneuverable aircraft technology (HiMAT) program explored the various and complex interactions of advanced technologies, such as aeroelastic tailoring, close-coupled canard, and relaxed static stability. A 0.44-subscale remotely piloted research vehicle (RPRV) of a hypothetical fighter airplane was designed and flight-tested to determine the effects of these interactions and to define the design techniques appropriate for advanced fighter technologies. Flexibility and high maneuverability were provided by flight control laws implemented in ground-based computers and telemetered to the vehicle control system during flight tests. The high quality of the flight-measured data and their close correlation with the analytical design modeling proved that the RPRV is a viable and cost-effective tool for developing aerodynamic, structure, and control law requirements for highly maneuverable fighter airplanes of the future.

  2. 76 FR 17986 - Public Notice for Waiver of Aeronautical Land-Use Assurance; Capital Region International Airport...

    Science.gov (United States)

    2011-03-31

    ... EXTENSION OF THE EASTERLY LINE OF CONSUMERS ENERGY PROPERTY AND ALONG SAID EASTERLY LINE, 502.24 FEET... SECTION 32; THENCE ALONG THE EASTERLY PROPOSED RIGHT-OF-WAY OF DEWITT ROAD RELOCATION FOR THE NEXT...

  3. 75 FR 16903 - Public Notice for Waiver of Aeronautical Land-Use Assurance Dayton-Wright Brothers Airport...

    Science.gov (United States)

    2010-04-02

    ...-of-way across said Grantor's 57.720 acre tract, to an iron pin set in the easterly line of Parcel 126...; Thence the following two (2) courses and distances along the easterly lines of said Parcel 126-WDV: 1. N... along the proposed north Right-of-way across said Grantor's 23.744 acre tract: 1. Easterly along arc...

  4. 75 FR 16899 - Public Notice for a Change in Use of Aeronautical Property at Houlton International Airport...

    Science.gov (United States)

    2010-04-02

    ... concrete monument at the most easterly corner of Lot 20 as shown on said Plan, said monument also marking... South 16 31'58'' East, a distance of 90.23 feet, more or less, to the intersection of the easterly limit... with the easterly limit of the right-of-way of Airport Drive; Thence, following the easterly limit...

  5. 76 FR 82031 - Public Notice for Waiver of Aeronautical Land-use Assurance; DuPage Airport, West Chicago, IL

    Science.gov (United States)

    2011-12-29

    .... 1633400, RECORDED MARCH 23, 1983 IN KANE COUNTY, ILLINOIS; THENCE EASTERLY ALONG THE EAST--WEST CENTERLINE... COUNTY, ILLINOIS; THENCE EASTERLY ALONG THE EAST--WEST CENTERLINE OF SAID SECTION 18, HAVING AN ILLINOIS... BEING A 2184.40 FEET RADIUS CURVE, CONCAVE SOUTHERLY; THENCE EASTERLY ALONG SAID NORTHERLY LINE AN...

  6. 77 FR 7231 - Public Notice for Release of Aeronautical Property at New Castle Airport (ILG), New Castle, DE

    Science.gov (United States)

    2012-02-10

    ... of Old Churchman's Road from Route 13 to the easterly boundary of the Thirty-Eight Acre Parcel, the... direction to the easterly property line of the Thirty-Eight Acre Parcel. The property is currently...

  7. An Initial Look at Adjacent Band Interference Between Aeronautical Mobile Telemetry and Long-Term Evolution Wireless Service

    Science.gov (United States)

    2016-07-04

    The three schemes are Quadrature Phase Shift Keying (QPSK), 16-Quadrature Amplitude Modulation (16-QAM), and 64-QAM. ADJACENT CHANNEL (BAND... noise power spectral density ratio (Eb/No). A difference of 1dB of required Eb/No to achieve an error rate of 1x10-5 as the victim is moved closer...distortion, the level of the AMT signal was minimized. The AMT waveform level was set approximately 20dB above where additive system noise was causing

  8. Fatigue FEM analysis in the case of brazed aluminium alloy 3L59 used in aeronautical industry

    Science.gov (United States)

    Dimitrescu, A.; Amza, Gh; Niţoi, D. F.; Amza, C. Gh; Apostolescu, Z.

    2016-08-01

    The use, on a larger scale, of brazed aluminum alloys in the aerospace industry led to the need for a detailed study of the assemblies behavior. These are built from 6061 aluminum aloy (3L59) brazed with aluminum aloy A103. Therefore, a finit element simulation (FEM) of durability is necessary, that consists in the observation of gradual deterioration until failure. These studies are required and are previous to the stage of the producing the assembly and test it by traditional methods.

  9. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) summer faculty fellowship program, 1986, volume 1

    Science.gov (United States)

    Mcinnis, Bayliss (Editor); Goldstein, Stanley (Editor)

    1987-01-01

    The Johnson Space Center (JSC) NASA/ASEE Summer Faculty Fellowship Program was conducted by the University of Houston. The basic objectives of the program are: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching objectives of participants' institutions; and (4) to contribute to the research objectives of the NASA Centers. Each faculty fellow spent ten weeks at JSC engaged in a research project commensurate with his interests and background and worked in collaboration with a NASA/JSC colleague. Volume 1 contains sections 1 through 14.

  10. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) summer faculty fellowship program, 1986, volume 2

    Science.gov (United States)

    Mcinnis, Bayliss (Editor); Goldstein, Stanley (Editor)

    1987-01-01

    The Johnson Space Center (JSC) NASA/ASEE Summer Faculty Fellowship Program was conducted by the University of Houston and JSC. The ten week program was operated under the auspices of the American Society for Engineering Education (ASEE). The basic objectives of the program are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objectives of the NASA Centers. Each faculty fellow spent ten weeks at JSC engaged in a research project commensurate with his interests and background and worked in collaboration with a NASA/JSC colleague. The final reports on the research projects are presented. This volume, 2, contains sections 15 through 30.

  11. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1987, volume 1

    Science.gov (United States)

    Jones, William B. (Editor); Goldstein, Stanley H. (Editor)

    1987-01-01

    The objective of the NASA/ASEE program were: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objectives of the NASA centers. Each faculty fellow spent 10 weeks at Johnson Space Center engaged in a research project commensurate with his/her interests and background and worked in collaboration with a NASA/JSC colleague. A compilation is presented of the final reports on the research projects done by the fellows during the summer of 1987. This is volume 1 of a 2 volume report.

  12. National Aeronautics and Space Administration (nasa)/american Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1991, Volume 1

    Science.gov (United States)

    Hyman, William A. (Editor); Goldstein, Stanley H. (Editor)

    1991-01-01

    Presented here is a compilation of the final reports of the research projects done by the faculty members during the summer of 1991. Topics covered include optical correlation; lunar production and application of solar cells and synthesis of diamond film; software quality assurance; photographic image resolution; target detection using fractal geometry; evaluation of fungal metabolic compounds released to the air in a restricted environment; and planning and resource management in an intelligent automated power management system.

  13. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1993, volume 1

    Science.gov (United States)

    Hyman, William A. (Editor); Goldstein, Stanley H. (Editor)

    1993-01-01

    The JSC NASA/ASEE Summer Faculty Fellowship Program was conducted by Texas A&M University and JSC. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are as follows: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participants' institutions; and (4) to contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA/JSC colleague. This document is a compilation of the final reports on the research projects completed by the faculty fellows during the summer of 1993.

  14. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1994, volume 1

    Science.gov (United States)

    Bannerot, Richard; Sickorez, Donn G.

    1995-01-01

    The JSC NASA/ASEE Summer Faculty Fellowship Program was conducted by Texas A&M University and JSC. The objectives of the program, which began nationally in 1964 and at JSC in 1965 are to: (1) further the professional knowledge of qualified engineering and science faculty members, (2) stimulate an exchange of ideas between participants and NASA, (3) enrich and refresh the research and teaching activities of participants' institutions, and (4) contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA JSC colleague. This document is a compilation of the final reports on the research projects completed by the faculty fellows during the summer of 1994.

  15. National Aeronautics and Space Administration (NASA)/american Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1991, Volume 2

    Science.gov (United States)

    Hyman, William A. (Editor); Goldstein, Stanley H. (Editor)

    1991-01-01

    The objectives of the program are: (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participant's institutions; and (4) to contribute to the research objectives of the NASA Centers. A compilation of the final reports on the research projects done by the faculty fellows during the summer of 1991 are presented. Some of the topics covered include: collision avoidance for rover vehicles, bioinstrumentation, neural nets, total quality management of flexible space structures, project scheduling, nondestructive tests, orthostatic intolerance to bedrest, hypersonic reentry simulation, measuring human energy expenditure, tribological models, trace element movement in Anarctic ice, gastrointestinal function, and computer assisted instruction.

  16. National Aeronautics and Space Administration (NASA)/American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program, 1993, volume 2

    Science.gov (United States)

    Hyman, William A. (Editor); Goldstein, Stanley H. (Editor)

    1993-01-01

    The JSC NASA/ASEE Summer Faculty Fellowship Program was conducted by Texas A&M University and JSC. The objectives of the program, which began nationally in 1964 and at JSC in 1965, are (1) to further the professional knowledge of qualified engineering and science faculty members; (2) to stimulate an exchange of ideas between participants and NASA; (3) to enrich and refresh the research and teaching activities of participant's institutions; and (4) to contribute to the research objectives of the NASA centers. Each faculty fellow spent at least 10 weeks at JSC engaged in a research project in collaboration with a NASA/JSC colleague. A compilation of the final reports on the research projects completed by the faculty fellows during the summer of 1993 is presented.

  17. Environmental statement for National Aeronautics and Space Administration, Office of Space Science, launch vehicle and propulsion programs

    Science.gov (United States)

    1972-01-01

    NASA OSS Launch Vehicle and Propulsion Programs are responsible for the launch of approximately 20 automated science and applications spacecraft per year. These launches are for NASA programs and those of other U. S. government agencies, private organizations, such as the Comsat Corporation, foreign countries, and international organizations. Launches occur from Cape Kennedy, Florida; Vandenberg Air Force Base, California; Wallops Island, Virginia; and the San Marco Platform in the Indian Ocean off Kenya. Spacecraft launched by this program contribute in a variety of ways to the control of and betterment of the environment. Environmental effects caused by the launch vehicles are limited in extent, duration, and intensity and are considered insignificant.

  18. Swamp Works: A New Approach to Develop Space Mining and Resource Extraction Technologies at the National Aeronautics Space Administration (NASA) Kennedy Space Center (KSC)

    Science.gov (United States)

    Mueller, R. P.; Sibille, L.; Leucht, K.; Smith, J. D.; Townsend, I. I.; Nick, A. J.; Schuler, J. M.

    2015-01-01

    The first steps for In Situ Resource Utilization (ISRU) on target bodies such as the Moon, Mars and Near Earth Asteroids (NEA), and even comets, involve the same sequence of steps as in the terrestrial mining of resources. First exploration including prospecting must occur, and then the resource must be acquired through excavation methods if it is of value. Subsequently a load, haul and dump sequence of events occurs, followed by processing of the resource in an ISRU plant, to produce useful commodities. While these technologies and related supporting operations are mature in terrestrial applications, they will be different in space since the environment and indigenous materials are different than on Earth. In addition, the equipment must be highly automated, since for the majority of the production cycle time, there will be no humans present to assist or intervene. This space mining equipment must withstand a harsh environment which includes vacuum, radical temperature swing cycles, highly abrasive lofted dust, electrostatic effects, van der Waals forces effects, galactic cosmic radiation, solar particle events, high thermal gradients when spanning sunlight terminators, steep slopes into craters / lava tubes and cryogenic temperatures as low as 40 K in permanently shadowed regions. In addition the equipment must be tele-operated from Earth or a local base where the crew is sheltered. If the tele-operation occurs from Earth then significant communications latency effects mandate the use of autonomous control systems in the mining equipment. While this is an extremely challenging engineering design scenario, it is also an opportunity, since the technologies developed in this endeavor could be used in the next generations of terrestrial mining equipment, in order to mine deeper, safer, more economical and with a higher degree of flexibility. New space technologies could precipitate new mining solutions here on Earth. The NASA KSC Swamp Works is an innovation environment and methodology, with associated laboratories that uses lean development methods and creativity-enhancing processes to invent and develop new solutions for space exploration. This paper will discuss the Swamp Works approach to developing space mining and resource extraction systems and the vision of space development it serves. The ultimate goal of the Swamp Works is to expand human civilization into the solar system via the use of local resources utilization. By mining and using the local resources in situ, it is conceivable that one day the logistics supply train from Earth can be eliminated and Earth independence of a space-based community will be enabled.

  19. Barriers to Fully Implementing Integrated Logistics Support (ILS) in System Acquisition as Perceived by ILS Managers and Program Managers at the Aeronautical Systems Division

    Science.gov (United States)

    1982-09-01

    brteen c• omands for ’experience trades.’ 122. SPO business is a crisis business. Logistics iswues do not reach a crisis stage ear)(, so we need an...Hans J., and David L. Wileman. "Conflict Management in Project Life Cycles," Sloan Management Review, XVI, No. 3 (Spriiig 1977), pp. 31-50. 33

  20. NASA University Research Centers Technical Advances in Aeronautics, Space Sciences and Technology, Earth Systems Sciences, Global Hydrology, and Education. Volumes 2 and 3

    Science.gov (United States)

    Coleman, Tommy L. (Editor); White, Bettie (Editor); Goodman, Steven (Editor); Sakimoto, P. (Editor); Randolph, Lynwood (Editor); Rickman, Doug (Editor)

    1998-01-01

    This volume chronicles the proceedings of the 1998 NASA University Research Centers Technical Conference (URC-TC '98), held on February 22-25, 1998, in Huntsville, Alabama. The University Research Centers (URCS) are multidisciplinary research units established by NASA at 11 Historically Black Colleges or Universities (HBCU's) and 3 Other Minority Universities (OMU's) to conduct research work in areas of interest to NASA. The URC Technical Conferences bring together the faculty members and students from the URC's with representatives from other universities, NASA, and the aerospace industry to discuss recent advances in their fields.