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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 2004-09-17T07:08:15Z
dc.date.available 2004-09-17T07:08:15Z
dc.date.issued 2002-08-05 en_US
dc.identifier.citation AIAA/AAS Astrodynamics Specialist Conference en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 02-1854 en_US
dc.identifier.uri http://hdl.handle.net/2014/9695
dc.description.abstract This paper describes the methods used to estimate the statistical delta V and propellant requirements for propulsive maneuvers necessary to deliver the two Rovers while ensuring that planetary protection requirements are satisfied. en_US
dc.format.extent 3376045 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other statistical delta V 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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