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Optimal low-thrust orbital transfers around a rotating non-spherical body

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dc.contributor.author Whiffen, Gregory J.
dc.date.accessioned 2005-12-09T17:17:31Z
dc.date.available 2005-12-09T17:17:31Z
dc.date.issued 2004-02
dc.identifier.citation 14th AAS/AIAA Space Flight Mechanics Meeting, Maui, HI, February 8-12, 2004 en
dc.identifier.clearanceno 04-0325
dc.identifier.uri http://hdl.handle.net/2014/38273
dc.description.abstract The NASA Discovery Program mission named DAWN will launch in 2006 to orbit the two giant asteroids Vesta and Ceres. The DAWN spacecraft will use solar-electric propulsion for both the interplanetary cruise and orbital operations at each asteroid. en
dc.description.sponsorship NASA en
dc.format.extent 1868007 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2004. en
dc.subject low-thrust en
dc.subject optimal control en
dc.subject asteroid en
dc.title Optimal low-thrust orbital transfers around a rotating non-spherical body en
dc.type Preprint en


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