Increasingly stringent thermal requirements are projected for future spacecraft. Compliance with these requirements necessitates the development of two-phase thermal control loops. These systems require a heat exchanger to couple the condenser section of the loop to a heat pipe radiator assembly. This paper presents a preliminary design of such a heat exchanger.


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    Title :

    A low pressure drop heat exchanger with integral heat pipe


    Additional title:

    Niederdruck-Tropfenwaermetauscher mit integralem Waermerohr


    Contributors:
    Fredley, J.E. (author) / Braun, C.E. (author)

    Published in:

    Publication date :

    1988


    Size :

    11 Seiten, 10 Bilder, 1 Tabelle, 10 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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