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.
Mars Pathfinder Spacecraft, Lander, and Rover Testing in Simulated Deep Space and Mars Surface Environments
1996-10-28
Miscellaneous
No indication
English
testing , environmental , Mars , thermal-vacuum , simulations , Pathfinder
British Library Conference Proceedings | 1997
|Mars Pathfinder Lander Deployment Mechanisms
British Library Conference Proceedings | 1996
|Mars Pathfinder Lander Deployment Mechanisms
NTRS | 1996
|