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 |