Scientific and Technical Aerospace Reports, 27. sējums,21-24. izdevumsScientific and Technical Information Office, National Aeronautics and Space Administration, 1989 Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database. |
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1.–5. rezultāts no 100.
2954. lappuse
... ENERGY PRODUCTION AND CONVERSION 3028 Includes specific energy conversion systems , e.g. , fuel cells ; global sources of energy ; geophysical conversion ; and windpower . For related information see also 07 Aircraft Propulsion and ...
... ENERGY PRODUCTION AND CONVERSION 3028 Includes specific energy conversion systems , e.g. , fuel cells ; global sources of energy ; geophysical conversion ; and windpower . For related information see also 07 Aircraft Propulsion and ...
2955. lappuse
... ENERGY PHYSICS Systers theory . For space radiation see 93 Space Radiation . 3046 74 OPTICS 3069 Includes light phenomena and optical devices . For lasers see 36 Lasers and Masers . 75 PLASMA PHYSICS AND SPACE POLICY Includes NASA ...
... ENERGY PHYSICS Systers theory . For space radiation see 93 Space Radiation . 3046 74 OPTICS 3069 Includes light phenomena and optical devices . For lasers see 36 Lasers and Masers . 75 PLASMA PHYSICS AND SPACE POLICY Includes NASA ...
2960. lappuse
... energy attenuating seats are used to provide a controlled deceleration over a vertical stroking distance to keep aircraft crash loads within human tolerance . Present energy attenuating crew seats use this approach of translating the ...
... energy attenuating seats are used to provide a controlled deceleration over a vertical stroking distance to keep aircraft crash loads within human tolerance . Present energy attenuating crew seats use this approach of translating the ...
2971. lappuse
... energy for orbital flight operations rather than photovoltaic solar array systems . To generate the current program baseline power of 75 kW , two or more solar concentrators approximately 50 feet in diameter would be required to replace ...
... energy for orbital flight operations rather than photovoltaic solar array systems . To generate the current program baseline power of 75 kW , two or more solar concentrators approximately 50 feet in diameter would be required to replace ...
2972. lappuse
... energy is available . Author N89-26894 * # Lockheed Missiles and Space Co. , Huntsville , AL . Engineering Center . SPACE SHUTTLE MAIN ENGINE STRUCTURAL ANALYSIS AND DATA REDUCTION / EVALUATION . VOLUME 7 : HIGH PRESSURE FUEL TURBO ...
... energy is available . Author N89-26894 * # Lockheed Missiles and Space Co. , Huntsville , AL . Engineering Center . SPACE SHUTTLE MAIN ENGINE STRUCTURAL ANALYSIS AND DATA REDUCTION / EVALUATION . VOLUME 7 : HIGH PRESSURE FUEL TURBO ...
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45 US dollars 80 Dutch guilders A01 CSCL Aeronautics and Space aircraft algorithm alloys analysis applications boundary layer California Inst components Contract Copyright Avail Dept developed dynamic effects Eggenstein-Leopoldshafen Electric Propulsion electron energy Engineering equations ESTEC European Space Agency evaluation experimental Final Report flow frequency Goddard Space Flight Greenbelt guilders or 45 heat Includes ion thruster Jet Propulsion Lab Laboratory for Oceans laser layer materials measurements mechanical method MPD thruster NASA National Aeronautics National Lab Naval Postgraduate School Netherlands Noordwijk NTIS HC A03/MF optical parameters percent performance physical plasma presented primary document Publications Div radiation related information Sandia National Labs satellite Science simulation solar Space Administration Space Flight Center Space Thermal Control spacecraft Spacecraft Propulsion structure superconducting Support Systems Dec surface Symposium on Space Tech Technical techniques Technology temperature Third European Symposium thruster Univ