A passive thermal system for use in satellites includes a solid radiator panel with a plurality of heat pipes attached to a surface thereof. In addition to their heat transporting capability, the heat pipes strengthen the radiator panel to which they are coupled. In some embodiments, the heat pipes are structurally modified to increase their area moment of inertia.


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    Titel :

    Satellite Radiator Panels with Combined Stiffener/Heat Pipe


    Beteiligte:
    SMITH ALEXANDER D (Autor:in) / FIELD DANIEL W (Autor:in) / ASKIJIAN ARMEN (Autor:in) / GROSSMAN JAMES (Autor:in)

    Erscheinungsdatum :

    06.10.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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