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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    Titel :

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


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Yendler, Boris (Autor:in) / Buchan, Eva (Autor:in) / Baumann, Jane (Autor:in) / Ambrose, Jay (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 2000



    Erscheinungsdatum :

    10.07.2000




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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