EPOXI Trajectory and Maneuver Analyses

Chung, Min-Kun J.; Bhaskaran, Shyamkumar; Chesley, Steven R.; Halsell, C. Allen; Helfrich, Clifford E.; Jefferson, David C.; McElrath, Timothy P.; Rush, Brian P.; Wang, Tseng-Chan M.; Yen, Chen-wan L.

NASA NTRS · 20150006807

EPOXI Trajectory and Maneuver Analyses

Chung, Min-Kun J.·Bhaskaran, Shyamkumar·Chesley, Steven R.·Halsell, C. Allen·Helfrich, Clifford E.·Jefferson, David C.·McElrath, Timothy P.·Rush, Brian P.·Wang, Tseng-Chan M.·Yen, Chen-wan L.

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Abstract

The EPOXI mission is a NASA Discovery Mission of Opportunity combining two separate investigations: Extrasolar Planet Observation and Characterization (EPOCh) and Deep Impact eXtended Investigation (DIXI). Both investigations reused the DI instruments and spacecraft that successfully flew by the comet Tempel-1 (4 July 2005). For EPOCh, the goal was to find exoplanets with the high resolution imager, while for DIXI it was to fly by the comet Hartley 2 (4 Nov 2010). This paper documents the navigation experience of the earlier ma-neuver analyses critical for the EPOXI mission including statistical ?V analyses and other useful analyses in designing maneuvers. It also recounts the trajectory design leading up to the final reference trajectory to Hartley 2.

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Chung, Min-Kun J., Bhaskaran, Shyamkumar, Chesley, Steven R., Halsell, C. Allen, Helfrich, Clifford E., Jefferson, David C., McElrath, Timothy P., Rush, Brian P., Wang, Tseng-Chan M., Yen, Chen-wan L.. 2011-07-31. EPOXI Trajectory and Maneuver Analyses. https://ntrs.nasa.gov/citations/20150006807

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