Parametric performance of extruded axial grooved heat pipes from 100to 300 K
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-724
Reference7 articles.
1. lilenas,T. A., and Howell, W. "Orbiting Astronomical Observatory Heat Pipes -Design, Analysis and Testing," ASME Paper No. 70HT/Sp 7-9.
2. Methane 100-130 1730 300 6100 1070 0.22-0.17 Ethane 150-225 1370 240
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