Voyager spacecraft phase B, task D. Volume 5 - Science payload integration Final report
Science experiments, photoimaging equipment, and Voyager spacecraft configurations for studying Mars atmosphere and surface temperature
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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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Science experiments, photoimaging equipment, and Voyager spacecraft configurations for studying Mars atmosphere and surface temperature
Design alternatives and growth potential of recommended and upgraded Voyager spacecraft configurations
Systems analysis and preliminary requirements for mission dependent and operational support equipment for Voyager Mars spacecraft
Dual mode hydrazine system for attitude control and maneuvering propulsion of interplanetary space probe
Hydrodynamical and mechanical design layout for two-speed hydraulic turbine inducer, computer simulation of pumping system and test facility performance, and study of demonstration unit
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