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New trajectory options for ballistic Mercury Orbiter Mission

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dc.contributor.author Yen, C. L. en_US
dc.date.accessioned 2004-09-22T22:22:54Z
dc.date.available 2004-09-22T22:22:54Z
dc.date.issued 2001-02-11 en_US
dc.identifier.citation 11th AAS/AIAA Space Flight Mechanics Meeting en_US
dc.identifier.citation Santa Barbara, California, USA en_US
dc.identifier.clearanceno 01-0123 en_US
dc.identifier.uri http://hdl.handle.net/2014/12195
dc.description.abstract This paper reports on recent advances made in obtaining low delta V trajectories to conduct Mercury orbiter missions. en_US
dc.format.extent 117259 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Mercury trajectory optimization en_US
dc.title New trajectory options for ballistic Mercury Orbiter Mission en_US


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