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Comet Ephemerides for the EPOXI and Stardust-NExT FlybysThe recently successful flybys of Comet 103P/Hartley 2 by the Deep Impact spacecraft and Comet 9P/Tempel 1 by the Stardust spacecraft each presented different challenges from the perspective of comet ephemeris prediction and spacecraft targeting. Hartley 2 is a small, highly active comet, with nongravitational accelerations that proved very difficult to model, requiring some amount of "cometchasing" by the spacecraft navigators. In contrast, Tempel 1 is a far larger and less active comet. It showed very stable ephemeris behavior and at flyby was within 1-sigma of predictions issued more than a year prior to encounter. This happenstance was fortuitous because the Stardust spacecraft had very little fuel margin available for comet ephemeris errors.
Document ID
20150007008
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Chesley, S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
April 30, 2015
Publication Date
October 3, 2011
Subject Category
Astronomy
Meeting Information
Meeting: European Planetary Science Congress (EPSC) Joint Meeting 2011
Location: Nantes
Country: France
Start Date: October 2, 2011
End Date: October 7, 2011
Sponsors: European Planetary Science Congress
Distribution Limits
Public
Copyright
Other
Keywords
non-gravitational accelerations
comet ephemerides

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