This paper describes modeling and test results for a two Loop Heat Pipes (LHP) with a condenser designed to be used in a deployable spacecraft radiator system. These units were provided by the two major commercial US vendors of LHPs. The condenser used is a freeze-tolerant, parallel-flow design based on the International Space Station (ISS) deployable radiator design. This condenser allows the deployable radiator to be utilized without freeze-protection heaters.


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    Title :

    Modeling and Test Results for Two Loop Heat Pipes with a Freeze-Tolerant Condenser


    Additional title:

    Sae Technical Papers


    Contributors:
    Yendler, Boris (author) / Buchan, Eva (author) / Baumann, Jane (author) / Ambrose, Jay (author)

    Conference:

    International Conference On Environmental Systems ; 2000



    Publication date :

    2000-07-10




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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