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Mars Exploration Rover heat rejection system performance - comparison of ground and flight dataThis paper will describe the various design modifications made on the MER HRS from that of Mars Pathfinder spacecraft. A description of the flight performance during the seven-month cruise of the spacecraft will be given. A comparison of the performance on the ground and the flight will be presented. Any significant deviation in the flight performance will be described.
Document ID
20060043765
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/38860
Authors
Ganapathi, Gani
Birur, Gajanana
Krylo, Robert
Tsuyuki, Glenn
Date Acquired
August 23, 2013
Publication Date
July 19, 2004
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 34th International Conference on Environmental Systems (ICES), Colorado Springs, Colorado
Start Date: July 19, 2004
End Date: July 22, 2004
Distribution Limits
Public
Copyright
Other
Keywords
heat rejection
Mars Exploration Rover (MER)
thermal analysis

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