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Loop Heat Pipe Applications for Thermal Control of Martian Landers/RoversIn early nineties Mars was designated as the planet to be explored. The present results of Mars program include the following: Background of Mars program. Thermal control design for Martian spacecraft. Loop heat pipe for Lander and Rover. Test results. and LHP applications for future Martian Lander and Rover.
Document ID
20010003945
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
Authors
Birur, Gaj (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Rodriquez, Jose (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Nikitkin, Michael (Dynatherm Corp. Hunt Valley, MD United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 10th Spacecraft Thermal Control Technology Workshop
Location: El Segundo, CA
Country: United States
Start Date: February 24, 1999
End Date: February 26, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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