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

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