Variable Conductance Heat Pipe for a Lunar Variable Thermal Link
Author:
Affiliation:
1. Advanced Cooling Technologies, Inc.
2. NASA Marshall Space Flight Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-5120
Reference6 articles.
1. W. G. Anderson, M. C. Ellis, and K. Walker, "Variable Conductance Heat Pipe Radiators for Lunar and Martian Environments,"SPESIF 2009, Huntsville, AL, February24 - 27,2009.
2. W. G. Anderson, J. R. Hartenstine, K. L. Walker, and J. T. Farmer, "Variable Thermal Conductance Link for Lunar Landersand Rovers,"8thIECEC,Nashville, TN, July25-28,2010.
3. Variable Conductance Heat Pipe Performance after Extended Periods of Freezing
4. Loop Heat Pipe with Thermal Control Valve for Variable Thermal Conductance
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