A spacecraft chassis includes a chassis body defined by first and second opposing sides bound by a perimeter, wherein at least one heat-generating component is configured to be secured directly to the chassis body, and at least one heat dissipating feature configured to radiate heat generated from the at least one heat-generating component into outer space.


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    Titel :

    Spacecraft chassis and component configuration


    Beteiligte:
    DUNFORD JOSHUA A (Autor:in) / SIMARD GARRETT P (Autor:in) / REINEMAN SAMUEL T (Autor:in) / READ MCKENZIE W (Autor:in) / CRABTREE BRENT (Autor:in)

    Erscheinungsdatum :

    05.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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