Variable Conductance Heat Pipes for Variable Thermal Links
Author:
Affiliation:
1. Advanced Cooling Technologies, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3541
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 Landers and Rovers,"8thIECEC,Nashville, TN, July25-28,2010.
3. Variable Conductance Heat Pipe Performance after Extended Periods of Freezing
4. Marcus, B. D. "Theory and Design of Variable Conductance Heat Pipes: Hydrodynamics and Heat Transfer," NASA Report No. NASA-CR-146195, April1971.
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