Present paper's purpose is to describe three Thermal Control Systems (TCSs) on base of Loop Heat Pipes (LHPs) that were realized in frame of “Mars-96” program. The main problems that were solved during the TCSs elaboration and some terrestrial tests' results will be also presented here below.
Loop Heat Pipes for Space Mission Mars 96
Sae Technical Papers
International Conference On Environmental Systems ; 1996
1996-07-01
Conference paper
English
Mission Performance of the GLAS Loop Heat Pipes - 7 Years In Orbit
British Library Conference Proceedings | 2010
|High Conductance Loop Heat Pipes for Space Application
American Institute of Physics | 2006
|High Conductance Loop Heat Pipes for Space Application
British Library Conference Proceedings | 2006
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