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Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system

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dc.contributor.author Birur, G. C. en_US
dc.contributor.author Sur, T. W. en_US
dc.contributor.author Paris, A. D. en_US
dc.contributor.author Shakkottai, P. en_US
dc.contributor.author Green, A. A. en_US
dc.contributor.author Haapanen, S. I. en_US
dc.date.accessioned 2004-09-22T23:56:31Z
dc.date.available 2004-09-22T23:56:31Z
dc.date.issued 2001-10-22 en_US
dc.identifier.citation SPIE International Symposium on Micromachining and Microfabrication en_US
dc.identifier.citation San Francisco, CA, USA en_US
dc.identifier.clearanceno 01-1612 en_US
dc.identifier.uri http://hdl.handle.net/2014/13080
dc.description.abstract This 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. en_US
dc.format.extent 1138706 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other microchannel microspacecraft thermal control elctronics cooling heat exchanger en_US
dc.title Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system en_US


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