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Venus and Mars gravity-assist trajectories to Jupiter using nuclear electric propulsion

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dc.contributor.author Parcher, Daniel W.
dc.contributor.author Sims, Jon A.
dc.date.accessioned 2005-09-15T21:39:52Z
dc.date.available 2005-09-15T21:39:52Z
dc.date.issued 2005-01
dc.identifier.citation 15th AAS/AIAA Space Flight Mechanics Meeting, Copper Mountain, CO, January 23-27-2005 en
dc.identifier.clearanceno 05-0211
dc.identifier.uri http://hdl.handle.net/2014/37506
dc.description.abstract Optimal low-thrust gravity-assist trajectories to Jupiter using nuclear electric propulsion are presented. en
dc.description.sponsorship NASA en
dc.format.extent 209768 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject Venus en
dc.subject Mars en
dc.subject gravity assist en
dc.subject trajectories en
dc.subject Jupiter en
dc.subject low thrust en
dc.title Venus and Mars gravity-assist trajectories to Jupiter using nuclear electric propulsion en
dc.type Preprint en


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