Thrusterless variation of space probe trajectories in the gravitational field of a planet through repeatedly swinging by the moons of the planet

Physics

Scientific paper

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Gravitational Effects, Orbit Calculation, Swingby Technique, Flyby Missions, Galilean Satellites, Kepler Laws, Orbital Elements, Rendezvous Trajectories

Scientific paper

In order to conserve on space probe fuel, a scheme for inducing alteration in the orbital elements of a spacecraft by playing on the gravitational fields of a planet and its moons is presented. The technique is based on a simplified model of motion for the moons and the probe. The moons are considered to be in a circular orbit on the equatorial plane of the planet. The calculation method is explained and demonstrated, taking a tour of the moons of Jupiter as an example.

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