A method for cooling a satellite system comprising configuring a plurality of fins to absorb and emit thermal radiation, wherein the ratio of absorptivity/emissivity is less than one; mechanically coupling the plurality of fins to the outside surface of a satellite, wherein the angle of the plurality of fins can be adjusted and controlled such that they can be stowed against the surface of the satellite or deployed; deploying the fins as necessary to expel heat from the satellite.


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    Titel :

    Deployable Heat Radiator System and Method for Small Satellite Applications


    Beteiligte:
    MILLER MARTIN F (Autor:in) / WAYNE DAVID T (Autor:in) / OBUKHOV DMITRIY I (Autor:in) / BOOK KEVIN (Autor:in)

    Erscheinungsdatum :

    28.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT / B64G Raumfahrt , COSMONAUTICS



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