Voyager spacecraft phase B, task D. Volume 4 - Engineering tasks. Book 5 - Photo imaging Final report
Alternate methods of performing photoimaging experiments of Martian surface from orbiting Voyager spacecraft
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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
Parametric analysis of Mars hard lander and preentry subsystems - computer programs for systems analyses
Design and performance characteristics of Mars hard lander capsule point designs, and criteria and mission constraints for capsules 1 and 2
Analytical design data for capsules 3 and 4 in the Mars hard lander study system
Engineering design of Mars hard lander capsules 5 and 6 and illustrations for increasing payload size
Supporting data for mission planning and design criteria of Mars hard landing system
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