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Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling systemThis paper presents background on the need for pumped liquid cooling systems for future micro/nano spacecraft and results from this ongoing numerical and experimental investigation.
Document ID
20060040364
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/13080
Authors
Birur, G. C.
Sur, T. W.
Paris, A. D.
Shakkottai, P.
Green, A. A.
Haapanen, S. I.
Date Acquired
August 23, 2013
Publication Date
October 22, 2001
Distribution Limits
Public
Copyright
Other
Keywords
microchannel microspacecraft thermal control elctronics cooling heat exchanger

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