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Flight path control strategies for the 2003 Mars Exploration Rover (MER) mission

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dc.contributor.author Raofi, B. en_US
dc.contributor.author Bhat, R. S. en_US
dc.contributor.author D'Amario, L. A. en_US
dc.date.accessioned 2004-09-22T21:34:52Z
dc.date.available 2004-09-22T21:34:52Z
dc.date.issued 2002-08-02 en_US
dc.identifier.citation AIAA/AAS Astrodynamics Conference en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 02-0303 en_US
dc.identifier.uri http://hdl.handle.net/2014/11726
dc.description.abstract The MER Project will launch two spacecraft (MER-A and MER-B) to Mars in 2003 with the objective of delivering two rovers to different landing sites on Mars to study the surface composition and to look for evidence of present or past water. en_US
dc.format.extent 2322342 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other statistical propellant planetary protection en_US
dc.title Flight path control strategies for the 2003 Mars Exploration Rover (MER) mission en_US


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