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Mars Pathfinder Atmosphere Entry Trajectory Design

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dc.contributor.author Spencer, David A. en_US
dc.date.accessioned 2004-10-02T23:18:10Z
dc.date.available 2004-10-02T23:18:10Z
dc.date.issued 1995-08 en_US
dc.identifier.citation Halifax, Canada en_US
dc.identifier.clearanceno 95-0980 en_US
dc.identifier.uri http://hdl.handle.net/2014/30387
dc.description.abstract The Mars Pathfinder spacecraft will enter the Martian atmosphere directly from the interplanetary trajectory, at a relatively high velocity. The design of the nominal entry trajectory, and the accurate determination of potential trajectory dispersions, is necessary for the development of the Pathfinder Entry, Descent, and Landing (EDL) System. en_US
dc.format.extent 459162 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Mars Pathfinder en_US
dc.title Mars Pathfinder Atmosphere Entry Trajectory Design en_US


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