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.
2958. lappuse
... increases from 0.00 to 0.15 . A tight binding method has been used to calculate the energy bands of InSe and the activation energy for motion of Li + in the Van der Waals gap of InSe . The increase in resistance of a lithium borate ...
... increases from 0.00 to 0.15 . A tight binding method has been used to calculate the energy bands of InSe and the activation energy for motion of Li + in the Van der Waals gap of InSe . The increase in resistance of a lithium borate ...
2962. lappuse
... increase in equivalent flat plate area which results in a 5 percent degradation in specific range at the recommended cruise airspeed , a 2 percent increase in fuel flow at the maximum endurance airspeed , and a 4 knot degradation in ...
... increase in equivalent flat plate area which results in a 5 percent degradation in specific range at the recommended cruise airspeed , a 2 percent increase in fuel flow at the maximum endurance airspeed , and a 4 knot degradation in ...
2964. lappuse
... increasing ; and ( 4 ) turbine temperature is beneath the maximum allowable limit . The backup system is used in ... increase significantly , thus assuredly maintaining GRA a sufficiently rich fuel / air mixture to promote ignition ...
... increasing ; and ( 4 ) turbine temperature is beneath the maximum allowable limit . The backup system is used in ... increase significantly , thus assuredly maintaining GRA a sufficiently rich fuel / air mixture to promote ignition ...
2966. lappuse
... increase in Ci , but , it does yield a large increase in lateral control response . An increase in aileron size and deflection along with some of the other suggested modifications would certainly approach the desired GRA goal . 09 ...
... increase in Ci , but , it does yield a large increase in lateral control response . An increase in aileron size and deflection along with some of the other suggested modifications would certainly approach the desired GRA goal . 09 ...
2970. lappuse
... increased budget stringency , the high cost of space transportation has prompted analysts to examine a wide variety of ... increase the understanding of the basic problems associated with this development . The state - space approach is ...
... increased budget stringency , the high cost of space transportation has prompted analysts to examine a wide variety of ... increase the understanding of the basic problems associated with this development . The state - space approach is ...
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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