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Long Term Life Testing of a Mechanically Pumped Cooled Loop for Spacecraft Thermal Control

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dc.contributor.author Birur, Gajanana C. en_US
dc.date.available 2004-09-26
dc.date.issued 1997-06-23 en_US
dc.identifier.citation Atlanta, Georgia, USA en_US
dc.identifier.clearanceno 97-0470 en_US
dc.identifier.uri http://hdl.handle.net/2014/22025
dc.description.abstract The Mars Pathfinder (MPF) Spacecraft launched to Mars in December 1996, uses a mechanically pumped loop to transfer dissipated heat from the insulated lander electronics to an external radiator. en_US
dc.format.extent 553889 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Thermal Control cooling loop en_US
dc.title Long Term Life Testing of a Mechanically Pumped Cooled Loop for Spacecraft Thermal Control en_US


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