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A mini loop heat pipe suitable for Mars roversThis paper describes the thermal design requirements, the thermal performance characteristics and the flight qualification program of a mini-LHP suitable for the Mars Rovers.
Document ID
20060030741
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Pauken, M. T.
Birur, G. C.
Novak, K. S.
Date Acquired
August 23, 2013
Publication Date
May 19, 2002
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
loop heat pipe Mars rover thermal control

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