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.
Citation: 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. Download Citation
Author(s):
Dmitri Kozmine, Konstantin Goncharov, Michael Nikitkin, Yuri F. Maidanik, Yuri G. Fershtater, Smirnov Fiodor
Affiliated:
Lavochkin Association, Institute of Thermal Physics
Pages: 8
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Control systems
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