Scientific and Technical Aerospace Reports Volume 38 October 6 ...

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Subject Categories of the Division A. Aeronautics Select a category to view the collection of records cited. N.A. means no abstracts in that category. 02 Aerodynamics 1 Includes aerodynamics of flight vehicles, test bodies, airframe components and combinations, wings, and control surfaces. Also includes aerodynamics of rotors, stators, fans and other elements of turbomachinery. For related information, see also 34 Fluid Mechanics and Heat Transfer. 03 Air Transportation and Safety 5 Includes passenger and cargo air transport operations; aircraft ground operations; flight safety and hazards; and aircraft accidents. Systems and hardware specific to ground operations of aircraft and to airport construction are covered in 09 Research and Support Facilities (Air). Air traffic control is covered in 04 Aircraft Communications and Navigation. For related information see also 16 Space Transportation and Safety; and 85 Technology Utilization and Surface Transportation. 04 Aircraft Communications and Navigation 12 Includes all modes of communication with and between aircraft; air navigation systems (satellite and ground based); and air traffic control. For related information see also 06 Avionics and Aircraft Instrumentation; 17 Space Communications; Spacecraft Communications, Command and Tracking, and 32 Communications and Radar. 05 Aircraft Design, Testing and Performance 13 Includes all stages of design of aircraft and aircraft structures and systems. Also includes aircraft testing, performance, and evaluation, and aircraft and flight simulation technology. For related information, see also 18 Spacecraft Design, Testing and Performance and 39 Structural Mechanics. For land transportation vehicles, see 85 Technology Utilization and Surface Transportation. 06 Avionics and Aircraft Instrumentation 18 Includes all avionics systems, cockpit and cabin display devices, and flight instruments intended for use in aircraft. For relatead information see also 04 Aircraft Communications and Navigation; 08 Aircraft Stability and Control; 19 Spacecraft Instrumentation and Astrionics; and 35 Instrumentation and Photography. 07 Aircraft Propulsion and Power 20 Includes prime propulsion systems and systems components, e.g., gas turbine engines and compressors; and onboard auxiliary power plants for aircraft. For related information see also 20 Spacecraft Propulsion and Power, 28 Propellants and Fuels, and 44 Energy Production and Conversion.
08 Aircraft Stability and Control 23 Includes flight dynamics, aircraft handling qualities; piloting; flight controls; and autopilots. For related information, see also 05 Aircraft Design, Testing and Performance and 06 Avionics and Aircraft Instrumentation. 09 Research and Support Facilities (Air) 27 Includes airports, runways, hangers, and aircraft repair and overhaul facilities, wind tunnels, water tunnels, and shock tubes; flight simulators; and aircraft engine test stands. Also includes airport ground equipment and systems. For airport ground operation see 03 Air Transportation and Safety. For astronautical facilities see 14 Ground Support Systems and Facilities (Space). Subject Categories of the Division B. Astronautics Select a category to view the collection of records cited. N.A. means no abstracts in that category. 12 Astronautics (General) 30 Includes general research topics related to space flight and manned and unmanned space vehicles, platforms or objects launched into, or assembled in, outer space; and related components and equipment. Also includes manufacturing and maintenance of such vehicles or platforms. For specific topics in astronautics see categories 13 through 20. For extraterrestrial exploration, see 91 Lunar and Planetary Science and Exploration. 13 Astrodynamics 32 Includes powered and free-flight trajectories; and orbital and launching dynamics. 14 Ground Support Systems and Facilities (Space) 33 Includes launch complexes, research and production facilities; ground support equipment, e.g., mobile transporters; and test chambers and simulators. Also includes extraterrestrial bases and supporting equipment. For related information see also 09 Research and Support Facilities (Air). 15 Launch Vehicles and Launch Operations 33 Includes all classes of launch vehicles, launch/space vehicle systems, and boosters; and launch operations. For related information see also 18 Spacecraft Design, Testing, and Performance; and 20 Spacecraft Propulsion and Power. 16 Space Transportation and Safety 34 Includes passenger and cargo space transportation, e.g., shuttle operations; and space rescue techniques. For related information, see also 03 Air Transportation and Safety and 15 Launch Vehicles and Launch Vehicles, and 18 Spacecraft Design, Testing and Performance. For space suits, see 54 Man/System Technology and Life Support.
Page 1 and 2: Scientific and Technical Aerospace
Page 3 and 4: Introduction Scientific and Technic
Page 5: Table of Contents Subject Divisions
Page 9 and 10: 25 Inorganic, Organic, and Physical
Page 11 and 12: Subject Categories of the Division
Page 13 and 14: 61 Computer Programming and Softwar
Page 15 and 16: 82 Documentation and Information Sc
Page 17 and 18: Document Availability Information T
Page 19 and 20: Avail: NASA Public Document Rooms.
Page 21 and 22: Hardcopy & Microfiche Prices Code N
Page 23 and 24: ALABAMA AUBURN UNIV. AT MONTGOMERY
Page 25 and 26: ��
Page 27 and 28: 20000091005 NASA Langley Research C
Page 29 and 30: ing actuator loading, control surfa
Page 31 and 32: 20000088689 Mitre Corp., McLean, VA
Page 33 and 34: 20000092117 Defence Science and Tec
Page 35 and 36: Authority (MWAA), which operates Re
Page 37 and 38: 20000092083 NASA Goddard Space Flig
Page 39 and 40: inspections and modifications neces
Page 41 and 42: This report documents the Moving Ma
Page 43 and 44: ment concept by demonstrating the e
Page 45 and 46: tionality to accomplish this task.
Page 47 and 48: The following research results are
Page 49 and 50: the minimum number of actuators req
Page 51 and 52: of the wing span away from the form
Page 53 and 54: at Mississippi State University, pr
Page 55 and 56: The weather data (including images
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20000094311 NASA Johnson Space Cent
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human travel into space and the pla
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20000088562 NASA Langley Research C
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Contract(s)/Grant(s): NAS9-17900; R
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different design alternatives to th
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This viewgraph presentation reviews
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20000091015 NASA Marshall Space Fli
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Rocket engine propellent injector d
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The particle simulations in a Varia
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20000093952 Sverdrup Technology, In
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and nonrecurring cost benefits. Ben
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20000092491 Texas A&M Univ., Dept.
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A method has been developed for the
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uses the mechanical properties of c
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20000092050 MRJ, Inc., USA Transpor
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20000093330 Tennessee Univ., Dept.
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duced plasma analysis system is dev
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20000089851 Pennsylvania State Univ
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In this study, the authors examine
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modynamic properties are reported f
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cate that sensitized stainless stee
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20000088588 Army Research Lab., Wea
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Alloys is presented, along with det
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tion on Shape memory and Superelast
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transport in low water content S-SE
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difference in the pressure dependen
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are bonded together by a matrix res
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y others) Stress was incorporated i
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growth surface reactions directly.
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gies and decomposes at similar temp
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20000088395 Naval Air Warfare Cente
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Meeting; October 1999; Volume 1, pp
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20000088407 Georgia Inst. of Tech.,
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A double reaction mechanism is used
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Contract(s)/Grant(s): N00014-95-1-1
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20000088422 Illinois Univ. at Urban
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20000088427 Illinois Univ. at Urban
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The objective of this work was to c
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20000089790 Army Research Lab., Abe
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20000089796 Army Research Lab., Wea
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equation (SE)-based model with a li
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kcal/mole. The analysis of the test
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ence of a nonzero temperature sensi
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that the requisite AG research need
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The objectives of the Engine Resear
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20000094281 BAE Systems, Rome, NY U
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The Department of Defense (DoD) is
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are conducted on the SQALE test dat
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all permutations of the two on scor
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20000091443 Karlsruhe Univ., Intera
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environment for airborne L-band VV-
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ing with analysis and numerical com
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20000088533 Princeton Univ., Dept.
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pumps, blowers or fans require only
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20000091678 Aerojet-General Corp.,
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above 300Torr, several local discha
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asymmetric current-voltage characte
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For long-duration space missions, t
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20000088675 Texas Univ., Austin, TX
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is necessary to fully account for t
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the random walk of the gyroscope bi
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show an example to introduce magnet
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servation data. Planning for the co
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was able to completely duplicate ac
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For excitation of Raman scattering
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20000094276 Aerosoft, Inc., Blacksb
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mized, and dependent upon the desig
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from the analytical model. The resu
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pump substituting the conventional
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The problem of sensor runout in mag
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20000089743 Kyushu Inst. of Tech.,
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39 STRUCTURAL MECHANICS ��
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(b) massive shear band formation at
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The present method is based on the
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power law dependence of the embedde
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20000088634 Geological Survey, Wate
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of simultaneously acquiring images
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associated creep rates. Three glaci
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Geochemical studies are fundamental
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implementation and basis for this c
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Report No.(s): Rept-5098-04; No Cop
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aly is 1.7 standard deviations from
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atio of NO and on the discharge cur
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46 GEOPHYSICS ��
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matrix has a nonporous texture simi
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Magnetic measurements taken by the
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Continent and eastward progression
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Models 20000088625 NASA Goddard Spa
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20000090514 NASA Goddard Space Flig
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Center, USA; Jedlovec, G. J., NASA
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of recurring (at least four occurre
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conditions during Spacelab, Biokosm
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all suppressed in the RWV bioreacto
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20000088577 Air Force Inst. for Env
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tion and their implications on crew
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20000089912 Krug Life Sciences, Inc
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20000094303 NASA Johnson Space Cent
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address human factor issues, and po
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in a long-duration environment, and
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functions such as life support and
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error, allows for processor mode se
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20000088570 Naval Postgraduate Scho
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problems including an overview of t
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Report No.(s): NASA/TM-2000-210361;
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e detected and removed from the bod
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As the Army enters the 2lst century
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62 COMPUTER SYSTEMS ��
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tion resources. They also are often
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tion with Centrum voor Wiskunde en
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The development of a computational
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outputs. The neural network is trai
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20000090653 Johns Hopkins Univ., De
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A study on the use of neural networ
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neous Elasticity Clements, David L.
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Technological advances have made at
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Report No.(s): PB2000-106588; No Co
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able. Since these are situations th
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A superconductive solenoid model co
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can lead to beam deflection or mode
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20000089822 Institut Franco-Alleman
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20000086205 Joint Inst. for Nuclear
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heavy ions and improved detection s
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During the current funding period,
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We calculated a temperature rise of
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Monte Carlo code have been made. Th
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Testing can be divided into two cat
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20000092198 Kanazawa Univ., Dept. o
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camera and computer processor. Seve
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The objectives of this program incl
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ses. Dry substrate etch with a Si/S
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density dn(sub e)-bar/dt was as hig
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this second model leads to the prop
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adjacent to the substrate can be so
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is one of the unique points of GTCS
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This was the reports of Yayoi Study
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20000092169 Kyushu Univ., Dept. of
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20000092193 Nagaoka Univ. of Techno
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20000094029 National Inst. for Fusi
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A cooperative project aiming at sup
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20000089859 North Carolina State Un
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20000092173 Yamanashi Univ., Facult
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20000094275 South Dakota School of
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allow small SUSY corrections to the
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p(sub T), and the J/psi decay angul
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20000091584 Caelum Research Corp.,
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The goal of this thesis is to analy
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only if it is known with certainty
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from the NIST database system, whic
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20000088604 Vanguard Research, Inc.
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X-ray telescopes. These telescopes
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Supernovae play a key role in the d
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20000092510 Smithsonian Astrophysic
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This talk will discuss the present
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We have detected four far-infrared
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the physical origin of the phenomen
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several 10 (exp 6) K, with a spatia
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much impact on density enhancement,
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In this work, we investigate the ef
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We review the sources of uncertaint
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In a previous paper we have discuss
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20000090641 Observatoire de Paris-M
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20000090650 California Univ., Berke
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(sub 0) = 50 kilometers per second
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20000090670 Turin Univ., Ist. di Fi
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Using the Long Wavelength Spectrome
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ing these results with the noise le
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lom, Larry, Geological Survey, USA;
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20000094220 California Inst. of Tec
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technologies were identified becaus
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With the launch of the Chandra X-ra
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93 SPACE RADIATION ��
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from ground-based observatories lie
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is partly due to simple differences
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20000092518 Smithsonian Astrophysic
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A ABILITIES, 128 ABLATION, 113 ABNO
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BODY SWAY TEST, 222 BODY TEMPERATUR
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CRAB NEBULA, 387 CRACK PROPAGATION,
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EULER EQUATIONS OF MOTION, 267 EURO
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HEATING EQUIPMENT, 293 HEAVY IONS,
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LASER WELDING, 166 LASERS, 168 LATE
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MULTIGRID METHODS, 267, 268 MULTILA
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PLASTIC PROPERTIES, 181 PLATES (STR
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SAMPLING, 336 SANDS, 206 SANDWICH S
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SUPERNOVA REMNANTS, 365, 366, 367,
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WIND VELOCITY MEASUREMENT, 27, 214
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Balakrishnan, R., 318 Balda, Juan C
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Chung, T. J., 155 Chyuan, Shing-Woe
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Freitas, Marcilio S. R., 244 Fremer
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Hurley, K., 372 Hurley, Kevin, 391
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Laille, A., 303 Lait, L. R., 199 La
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Mora, K. L., 186 Morales, R., 369 M
Page 451 and 452:
Reda, Daniel C., 84 Reddy, J. N., 5
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Sture, Stein, 206 Sturm, James C.,
Page 455:
Wu, Z. Y., 170 PA-18 X Xia, W., 99
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