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Trajectory design for the Mars Reconnaissance Orbiter mission

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dc.contributor.author Halsell, C. A. en_US
dc.contributor.author Bowes, A. L. en_US
dc.contributor.author Johnston, M. D. en_US
dc.contributor.author Lyons, D. T. en_US
dc.contributor.author Lock, R. E. en_US
dc.contributor.author Xaypraseuth, P. en_US
dc.contributor.author Bhaskaran, S. en_US
dc.contributor.author Highsmith, D. E. en_US
dc.contributor.author Jah, M. K. en_US
dc.date.accessioned 2004-09-16T21:26:50Z
dc.date.available 2004-09-16T21:26:50Z
dc.date.issued 2003-02-10 en_US
dc.identifier.citation 13th AAA/AISS Space Flight Mechanics Meeting en_US
dc.identifier.citation Ponce, Puerto Rico en_US
dc.identifier.clearanceno 03-0327 en_US
dc.identifier.uri http://hdl.handle.net/2014/6542
dc.description.abstract This paper describes the analysis and design evolution of the Mars Reconnaissance Orbiter trajectory from launch to end-of-mission. en_US
dc.format.extent 3954821 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other trajectory design MRO Mars en_US
dc.title Trajectory design for the Mars Reconnaissance Orbiter mission en_US


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