Conceptual design of a Manned-Unmanned Lunar Explorer /MULE/
Manned-unmanned lunar explorer systems design
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Manned-unmanned lunar explorer systems design
Analytic procedures and computer codes for prediction of weight optimized radioisotope thermoelectric generator shields for unmanned spacecraft
Design of control equipment for unmanned Martian roving vehicle
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - summary
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - technical details
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - appendices
Development, definition, and characteristics of remote sensors for unmanned spacecraft conducting planetary exploration
Elevation determination methods for unmanned lunar roving vehicle, considering instruments, orbiter tracking, etc
Unmanned lunar roving vehicle remote guidance, discussing onboard vs on-earth steering and velocity control, imaging system, obstacle detection and avoidance
Thermionic reactor electric propulsion for unmanned outer planets exploration, discussing spacecraft design, launch vehicle, weight factors, etc
Unmanned lunar logistics vehicle for extended manned lunar exploration support, discussing general design, propulsion and control systems
Radioisotope thermionic power supply for unmanned electric propulsion missions to outer planets, using 69 modules consisting of thermionic converter and emitter heat pipe
Planetary quarantine analysis for unmanned Mars orbiter, considering accidental spacecraft impact, loose particles and gases used for attitude control and pressurization
Earth-spacecraft radio communication requirements for future unmanned planetary missions, emphasizing imaging experiments and sensors
Unmanned lunar rover exploration objectives and requirements, considering heterogeneous surface
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.
The guidance and navigation requirements for unmanned missions to the outer planets, assuming constant, low thrust, ion propulsion are discussed. The navigational capability of the ground based Deep Space Network is compared to the improvements in navigational capability brought about by the addition of guidance and navigation related onboard sensors. Relevant onboard sensors include: (1) the optical onboard navigation sensor, (2) the attitude reference sensors, and (3) highly sensitive accelerometers. The totally ground based, and the combination ground based and onboard sensor systems are compared by means of the estimated errors in target planet ephemeris, and the spacecraft position with respect to the planet.
The results of a study to determine the support requirements for remote sensor systems on unmanned planetary flyby and orbiter missions are presented. Sensors and experiment groupings for selected missions are also established. Computer programs were developed to relate measurement requirements to support requirements. Support requirements were determined for sensors capable of performing required measurements at various points along the trajectories of specific selected missions.