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Loop Heat Pipes for Space Mission Mars 96
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English
Abstract
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.
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Kozmine, D., Goncharov, K., Nikitkin, M., Maidanik, Y. et al., "Loop Heat Pipes for Space Mission Mars 96," SAE Technical Paper 961602, 1996, https://doi.org/10.4271/961602.Also In
References
- Meyer R. Muller R. Beckman K. Goncharov K.A. Kolyarov E.Yu. Maidanik Yu. F. “Investigation of the Heat Transfer Performance of a Capillary Pumped Ammonia Loop Under Gravity” 23rd International Conference on Environmental Systems Colorado Springs July 12-15 1993 paper 932304
- Goncharov K.A. Kotlyarov E. Yu. Smirnov F. Yu. Schlitt R. Beckman K. Meyer R. Muller R. “Investigation of Temperature Fluctuations in Loop Heat Pipes” 24th International Conference on Environmental Systems and 5th European Symposium on Space Environmental Control Systems Friedrichshafen June 20-23 1994 paper 941577