Mars Pathfinder mechanically pumped cooling loop

Birur, G. C.

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