Solar-electric-propulsion systems for unmanned space missions.
Electric propulsion ion engine systems using solar power source for Mars and Jupiter exploratory unmanned spacecraft is adaptable to existing launch vehicles
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Electric propulsion ion engine systems using solar power source for Mars and Jupiter exploratory unmanned spacecraft is adaptable to existing launch vehicles
Simulation of on-board multiprocessor for long lived unmanned space satellite control
Analytical evaluation of space storable propellants for unmanned Jupiter and Saturn orbiter missions
Pathfinding algorithm for unmanned roving vehicle to explore Martian surface
Analysis of propellant sensitivity, secondary propulsion, and ground operations for unmanned spacecraft propulsion systems
Feasibility of common stage for alternate space missions and attitude control systems for unmanned spacecraft propulsion system
Longitudinal range dispersion of unmanned Mars landers using VM-8 and VM-9 atmospheric models, discussing Syrtis Major as possible landing site
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
Mars unmanned spacecraft mission profiles for surface imaging, noting influence of lighting requirements
Direct flight and Jupiter swingby heliocentric trajectory modes of elliptic capture orbits compared for unmanned missions to outer planets
Systems safety for unmanned spacecraft, considering power supply, equipment operation, trajectory correction, etc
Prior to the establishment of a manned lunar observatory or base, it is essential that a compendium of information be available on the environment, composition, structure, and topography of the moon. In an effort to satisfy this need for improved and detailed information, NASA has undertaken a lunar program which ranges from the utilization of circumlunar flight vehicles, equipped with automatic photographic and radiation measuring equipment which responds to commands from the earth, to actual determination of surface composition and features obtained from unmanned instrumented spacecraft which impact the moon.
Design of thermionic reactor power systems for nuclear electric propelled unmanned spacecraft
Design calculations for magnetohydrodynamic power conversion system for nuclear electric propelled unmanned spacecraft
Analytic procedures and computer codes for predicting weight optimized radioisotope thermal generator shields for unmanned spacecraft
Planetary soil sampler prototypes for biological studies from unmanned space probes
Lift-drag ratio for out-of-orbit and direct entry modes for unmanned Viking class Mars landers
Observation requirements for unmanned planetary missions