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Results for “feasibility” Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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At least 937 records · Page 52NASA NTRS 1969
Solid state chemical heat sources aboard unmanned planetary landing vehicles to maintain batteries and experiments operability during cold planetary nights
NASA NTRS 1969
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NASA NTRS 1968
Radio frequency mass gaging technique model for particular spacecraft fuel and tank configuration
NASA NTRS 1968
Fuel gage configuration for Apollo spacecraft and lunar module propellant tanks
NASA NTRS 1969
Airborne Range and Orbit Determination as satellite geodetic survey instrument
NASA NTRS 1969
Compression molding technique for manufacturing Pyrrone pellets by isostatic pressing
NASA NTRS 1967
Resonant infrasonic gauging system investigated for Apollo project propulsion system
NASA NTRS 1969
Chemical and physical properties of ethylene glycol and silica gel adsorbent
NASA NTRS 1969
Infrared source for simulating earthshine radiation in thermal-vacuum chamber
NASA NTRS 1970
Remote sensing of atmospheric turbulence profiles
NASA NTRS 1969
Computerized design of photographic masks for integrated circuit fabrication
NASA NTRS 1969
Using combinations of heat and radiation for spacecraft sterilization
NASA NTRS 1970
Acoustic liner for controlling combustion instability in rocket engines using ablative chambers
NASA NTRS 1967
Manual completion of lunar orbit insertion burn with inertial measuring unit drifting about pitch axis
NASA NTRS 1970
Low temperature semiconductor deposition techniques in fabricating thick film, insulated gate, field effect transistors
NASA NTRS 1970
Design and construction of microbial ecology evaluation device for studying mutations on space missions
NASA NTRS 1970
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical heat transfer analysis
NASA NTRS 1970
V/STOL concepts for short haul commercial aircraft compared for gross weight, operating cost, gust sensitivity and noise levels