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Active heat rejection system on Mars Exploration Rover - design changes from Mars PathfinderThe 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.
Document ID
20210001966
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Patzold, J. D.
McGrath, P. L.
Tsuyuki, G. T.
Birur, G. C.
Ganapathi, G. B.
Date Acquired
February 2, 2003
Publication Date
February 2, 2003
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
spacecraft
thermal
control
advanced
thermal
control
technologies

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