dc.contributor.author |
Johnson, Kenneth R. |
en_US |
dc.date.accessioned |
2004-09-30T23:23:48Z |
|
dc.date.available |
2004-09-30T23:23:48Z |
|
dc.date.issued |
1996-10-28 |
en_US |
dc.identifier.citation |
Baltimore, MD |
en_US |
dc.identifier.clearanceno |
96-1386 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/26510 |
|
dc.description.abstract |
This paper describes the test program which was conducted to verify the Mars Pathfinder spacecraft thermal design. The testing program required subjecting the mission hardware to both deep space and Mars surface conditions. |
en_US |
dc.format.extent |
1360138 bytes |
|
dc.format.mimetype |
application/pdf |
|
dc.language.iso |
en_US |
|
dc.subject.other |
environmental testing Mars Pathfinder simulations thermal-vacuum testing |
en_US |
dc.title |
Mars Pathfinder Spacecraft, Lander, and Rover Testing in Simulated Deep Space and Mars Surface Environments |
en_US |