Sterilization Assembly Development Laboratory, 3000 cu ft decontamination chamber. Physical parameters - Measurement plan, task 1.0
Ethylene oxide concentration, humidity, time, and temperature parameters for large decontamination chamber
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Ethylene oxide concentration, humidity, time, and temperature parameters for large decontamination chamber
Design parameters and breadboard models for advanced soil samplers
Solar Energy Thermionic /SET/ generator design using converters with rhenium emitters
Potential flight management problems during low visibility landing of supersonic transports
Rotation and sinusoidal perturbation effects on astronauts executing perceptual motor tests in rotogravity space station
Computer system VISTA, automatically plots selective PERT networks in order to develop accurate, standardized scheduling documentation as an essential element to project planning. This automation of plotting networks generates standardized networks due to a priority scheme adopted for calculating paths between events.
Trends in commercial aircraft engine noise, performance, and dimensions as influenced by engine thermodynamic cycle variations
Design and performance of four candidate commercial aircraft engines
Aerodynamic commercial aircraft engine design for minimum noise level
Biomedical applications of aerospace generated technology
Spacecraft subsystem performance deterioration caused by nuclear radiation on space missions
Space probes with low magnetic interference to determine interplanetary magnetic fields
Analyses of unmanned space missions to Jupiter and outer planets
Volt-ampere characteristics improvement and life testing of electrodes for hydrogen oxygen fuel cells
Radioisotope thermoelectric generator interface specifications - NASA Evaluation With Models Of Optimized Nuclear Spacecraft /NEW MOONS/
Launch vehicle guidance and control requirements for unmanned space missions - Vol. 2, Part 1
Atlas and Saturn vehicle launch data for radio optical strapdown inertial guidance system study