Lunar drill feasibility study Final report
Low thrust rotary and percussive drills for sampling lunar surface
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Low thrust rotary and percussive drills for sampling lunar surface
Turboprop, fan-in-wing, and propulsive wing concepts for V/STOL commercical transport aircraft
Thin film oxygen partial pressure sensor
Advanced space environmental effects sensor using active control of sensor temperature
Mobility and structural analyses of bellows concept for lunar roving vehicle
Freeze-out technique for control of trace contaminants within manned spacecraft atmospheres
Method for physical recovery of carbon dioxide from space cabin atmosphere and chemical recovery of metabolic oxygen
Use of thermally-induced straining for grain refinement in recrystallized tungsten
Weight reductions in Saturn V thrust structure by using lightweight high strength beryllium blind and semi-blind fasteners
High altitude atmospheric density measurements using X-ray or gamma ray backscatter and rocket sounding techniques
Thin film tunnel cathodes evaluated for use in ultrahigh vacuum gauges
Water-filled capillary pumped heat transfer loops for removal of waste heat from spacecraft power devices
Fluidic control subsystem, describing components such as electric/fluid and position transducer, operational amplifier, fluid bellows and operation characteristics
Potential application of propulsion to aeronomy satellites
Piezojunction effect and silicon needle considered as sensory devices in accelerometers and transducers
X-ray collectors and detectors evaluated for use as spectrography experiment in Orbiting Astronomical Observatory /OAO/
Miniaturizing automatic amino acid analyzer for Apollo and Voyager missions
Vacuum pressure measurement beneath and within battens of high performance insulation on cryogenic storage tank