A study of space mission duration extension problems, volume 3
Availability concept as systems design tool for determining safe and effective long duration planetary flyby and return mission using contemporary hardware
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Availability concept as systems design tool for determining safe and effective long duration planetary flyby and return mission using contemporary hardware
Impulsive velocity requirements within Mars sphere of influence for converting stopover to powered flyby mission
Missions for solar-electric propulsion spacecraft, calculating flyby and elliptic capture missions to Jupiter, Saturn, Uranus and Neptune
Sun-Mars mass ratio solution by analysis of Mariner 4 flyby coherent Doppler tracking data
Data return advantages of earth-Mars-earth flyby trajectories over more conventional Mars trajectories
Lunar photographic methods and data including flyby, impacter, lander and orbiter photographic missions
JPL Solar Electric 1975 Jupiter Flyby program designed to minimize risks of introducing prime solar electric propulsion into spacecraft
Asteroid mission objectives and requirements, discussing asteroid lander and flyby missions
Launch window variation using circular and elliptical parking orbits and transfer techniques, discussing Venus and Mars flyby missions
Spacecraft guidance analysis of mulitiple outer planet mission utilizing gravity assist swingbys to achieve planetary flybys with single spacecraft
Mariner Mars 1969 flyby missions objectives, experiments, spacecraft configuration, trajectory design, sterilization, flight path control and photographic imaging
Solar electric power system for ion propelled Jupiter flyby mission, noting photovoltaic solar array, battery energy storage and power conditioning
Mariner Mars flyby mission 1969, discussing two spacecraft launching, mission objectives and launch-return flight design
Mariner spacecraft design and technology for Mars flyby in 1969 noting data storage, planetary scan, power subsystem, sequencer, telemetry and packaging
Development of optimum Mariner spacecraft power system for application to future flyby and orbiter missions
Design and hardware of restraining and deploying mechanism for solar array of Mars flyby mission
Close flyby trajectory calculations around planets with return to earth capability