Solar electric earth gravity assist /SEEGA/ missions to the outer planets

Computer Science – Performance

Scientific paper

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Astrodynamics, Interplanetary Trajectories, Mission Planning, Outer Planets Explorers, Solar Electric Propulsion, Swingby Technique, Trajectory Optimization, Circular Orbits, Earth Orbits, Geopotential, Graphs (Charts), Planetary Orbits, Saturn (Planet), Space Shuttles

Scientific paper

The optimization of solar electric propulsion earth-gravity-assist trajectories to the outer planets is presented. Included in the optimization is both earth swingby velocity and swingby date. Mission modes with and without optimal post swingby thrust are compared. Performance suitable for preliminary mission studies is presented for the four major outer planets using circular-coplanar planetary orbits and additional performance is presented for a Saturn Orbiter-Dual Probe mission.

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