Earth revolution synchronous orbits and aero-gravity assists to enhance capabilities for interplanetary missions by sub-payload spacecraft

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Ogawa, Naoko
Mimasu, Yuya
Tanaka, Keita
Yamaguchi, Tomohiro
Fujita, Kazuhisa
Narita, Shinichiro
Kawaguchi, Jun'ichiro

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This paper proposes a strategy for sub-payload spacecraft to extend possibility of interplanetary exploration without interrupting the mission by the main spacecraft. Combination of Earth revolution synchronous orbits and aero-gravity assists at Earth will allow sub-payload spacecraft to control its departure timing, C3 energy and destination independently. A case study of a possible sub-payload bound for Mars is shown and a preliminary mission sequence is presented.

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Space for Our Future - Advances in the Astronautical Sciences: Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012

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