NASA NTRS · 20060036278
Integrated Thermal Control for Mars Rover
Abstract
The Mars Rover has been built, environmentally tested and qualified for the 1996 launch of the Pathfinder mission to Mars. The basic structure for the thermal control for the Mars Rover is the Warm Electronics Box (WEB). This consists of a thermal isolating composite structure with co-cured thermal control surfaces and an ultralightweight hydrophobic solid silica aerogel which minimizes conduction and radiation.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Hickey, Gregory S., Braun, David, Wen, Liang-Chi, Eisen, Howard J.. 1996-07-10. Integrated Thermal Control for Mars Rover. https://ntrs.nasa.gov/citations/20060036278
Cite the original work for its findings. Save a collection to share your selection of sources.