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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    Title :

    Loop Heat Pipes for Space Mission Mars 96


    Additional title:

    Sae Technical Papers



    Conference:

    International Conference On Environmental Systems ; 1996



    Publication date :

    1996-07-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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