Comparison of small water-graphite nuclear rocket stages with chemical upper stages for unmanned missions
Small water-graphite nuclear rocket stages compared with chemical upper stages for use in unmanned spacecraft
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Small water-graphite nuclear rocket stages compared with chemical upper stages for use in unmanned spacecraft
Self-synchronizing, biorthogonal coded pulse code modulation telemetry system for communicating with unmanned spacecraft
Electric propulsion ion engine systems using solar power source for Mars and Jupiter exploratory unmanned spacecraft is adaptable to existing launch vehicles
Computational requirements and information storage devices for unmanned spacecraft in advanced planetary exploration, 1975 - 1985
Design of space simulator for environmental testing of unmanned spacecraft
Lightly loaded truss structures fabricated from Be, Be-Al alloy and uniaxial B filament reinforced epoxy tubing for unmanned spacecraft applications
Martian surface minerological study of present state and past processes from rock analyses by unmanned spacecraft instruments to test planetary models
Deep Space Network for two-way communications with unmanned spacecraft at planetary distances - Vol. 2
Photosensitive light source device for detecting unmanned spacecraft deviation from reference attitude
High Energy Astronomy Observatory for space X rays, gamma and cosmic rays research via unmanned spacecraft
Development and characteristics of electric propulsion systems for manned and unmanned spacecraft
Malfunctions and failures in first-day performance of 57 unmanned spacecraft
Design, development, and operation of communications system for command and control of unmanned spacecraft during exploration of deep space
Development, definition, and characteristics of remote sensors for unmanned spacecraft conducting planetary exploration
Thermal scale modeling limitations for radiation- conduction system of unmanned spacecraft, discussing material thermal properties, model dimensions, instrumentation effects and environment simulation
Unmanned spacecraft first day failures, discussing launch environment, duration tests in simulated space and performance improvement
Scientific, unmanned spacecraft on mission to Jupiter and beyond will be subjected to nuclear radiation from the natural environment and onboard nuclear power sources which may be harmful to subsystems. This report postulates these environments and discusses practical considerations to ensure confidence that the spacecraft's materials and subsystems will withstand the effects of anticipated radiation. Degradation mechanisms are discussed.
Unmanned spacecraft missions to the outer planets are of current interest to planetary scientists, and are being studied for the post 1970 time period. Flyby, entry and orbiter missions are all being considered using both direct and planetary swingby trajectory modes. The navigation and guidance requirements for a variety of missions to the outer planets and comets including both the three and four planet Grand Tours, are summarized.