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Active heat rejection system on Mars Exploration Rover - design changes from Mars Pathfinder

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dc.contributor.author Ganapathi, G. B. en_US
dc.contributor.author Birur, G. C. en_US
dc.contributor.author Tsuyuki, G. T. en_US
dc.contributor.author McGrath, P. L. en_US
dc.contributor.author Patzold, J. D. en_US
dc.date.accessioned 2004-09-17T19:00:01Z
dc.date.available 2004-09-17T19:00:01Z
dc.date.issued 2003-02-02 en_US
dc.identifier.citation Space Technology and Application International Forum en_US
dc.identifier.citation Albuquerque, NM, USA en_US
dc.identifier.clearanceno 02-2679 en_US
dc.identifier.uri http://hdl.handle.net/2014/10604
dc.description.abstract The active Heat Rejection System designed for Mars Pathfinder was modified for the Mars Exploration Rover mission and will be used to remove excess heat from the Rover electronics during the cruise part of the mission. This paper addresses the lessons learned from the performance testing, and potential changes to improve the HRS performance. en_US
dc.format.extent 3390138 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other spacecraft thermal control advanced thermal control technologies en_US
dc.title Active heat rejection system on Mars Exploration Rover - design changes from Mars Pathfinder en_US


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