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Preliminary Design of Low-Thrust Interplanetary Missions

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dc.contributor.author Sims, J. en_US
dc.contributor.author Flanagan, S. en_US
dc.date.accessioned 2004-09-24T16:36:53Z
dc.date.available 2004-09-24T16:36:53Z
dc.date.issued 1999-08-16 en_US
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference en_US
dc.identifier.citation Girdwood, Alaska, USA en_US
dc.identifier.clearanceno 99-1373 en_US
dc.identifier.uri http://hdl.handle.net/2014/17923
dc.description.abstract A direct optimization method intended to be used primarily for preliminary design of low-thrust interplanetary trajectories, including those with multiple gravity assists, is presented. en_US
dc.format.extent 758509 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other trajectory interplanetary low-thrust preliminary design en_US
dc.title Preliminary Design of Low-Thrust Interplanetary Missions en_US


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