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

Parcher, Daniel W.; Sims, Jon A.

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