The development of a thermal control system for a spacecraft module is discussed. The wall structures are composed of superinsulation in some cases and of thermally conductive material in other cases. Heat pipes are installed to provide a path of heat transfer from the interior of the module to space. The design of the system makes it possible to maintain a relatively uniform temperature throughout the module with side variations of the amount of heat dissipated by the components within the module.


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    Titel :

    Thermal control system for a spacecraft modular housing


    Beteiligte:
    Eby, R. J. (Autor:in) / Powers, E. I. (Autor:in)

    Erscheinungsdatum :

    1973-07-31


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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