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Mars Pathfinder mechanically pumped cooling loop

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dc.contributor.author Birur, G. C. en_US
dc.contributor.author en_US
dc.date.accessioned 2004-09-23T16:54:59Z
dc.date.available 2004-09-23T16:54:59Z
dc.date.issued 2001-06-28 en_US
dc.identifier.citation Pasadena, CA, USA en_US
dc.identifier.clearanceno 01-1477 en_US
dc.identifier.uri http://hdl.handle.net/2014/13633
dc.description.abstract A mechanically pumped single-phase cooling loop was successfully flown on the Mars Pathfinder (MPF) Spacecraft which safely landed on the Martian surface on July 4, 1997. One of the key technologies that enabled the mission to succeed was an active heat rejection system (HRS) used to cool the electronics on the spacecraft during its seven-month cruise from Earth to Mars. en_US
dc.format.extent 3774361 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other spacecraft tehermal control pumped cooling loop en_US
dc.title Mars Pathfinder mechanically pumped cooling loop en_US


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