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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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Flight dynamics, experiment operational phase sequence, and support operations for Applications Technology Satellite /ATS/ MISSION
Manned orbital research laboratory mission planning analysis
Design and material evaluation program for fabrication of large ablative motor nozzle and exit cone
Applicability of Saturn/Apollo checkout system and support equipment to Voyager project
Comparative evaluation of centralized versus decentralized computer system for digital data processing on Voyager spacecraft
Chemical kinetics analysis of Mars atmosphere composition and physical properties
Alternate methods of performing photoimaging experiments of Martian surface from orbiting Voyager spacecraft
Effect of radioisotope thermal generators in flight capsule on Voyager spacecraft configuration
Voyager spacecraft configuration, systems and trajectory analyses, and system integration interfaces
Functional descriptions, interfaces, performance, and physical characteristics of Voyager 1973 flight spacecraft telecommunication system
Baseline design and functional requirements of Voyager spacecraft guidance and control, computer and sequencer, and power subsystems, and electrical system
Structural design and engineering mechanics of baseline Voyager spacecraft, propulsion support, and planetary scan platform
Voyager spacecraft design standards, and operational support and mission-dependent equipment requirements
Systems engineering and constraints, cost estimates, and program schedule for Venus flyby/entry probe mission
Vibration, shock, and acceptance test data for C-1 rocket engine propellant valve qualification
Specifications, design concepts, and qualification test procedures for C-1 engine bipropellant valve
Structural design, systems and subsystems requirements, entry probe configurations, and transfer trajectories for flyby/entry probe system for 1972 Venus launch
Mission lander maps for parametric data, entry aeroshell, and parachute subsystem used in Mars hard lander study