An apparatus comprising a satellite includes a first radiator panel on a first side of a central body of the satellite and a second radiator panel on a second side of the central body is provided. The first radiator panel is thermally attached to the second radiator panel. A third side of the central body is positioned between the first side and the second side. A fourth side of the central body is positioned between the first side and the second side, opposing the third side. The first radiator panel is thermally attached to the second radiator panel by one or more coupling heat pipes, the coupling heat pipes exposed to an exterior environment of the satellite.


    Access

    Download


    Export, share and cite



    Title :

    RADIATING COUPLING HEAT PIPE


    Contributors:

    Publication date :

    2023-10-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / 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



    Reversible loop heat pipe layout for satellite radiating surface coupling

    XIE LONG / ZHAO JIELIAN / NIU LEI | European Patent Office | 2022

    Free access

    Thickened radiating pipe of heat exchanger and using method

    QIN WENMING / CHEN XIANGLONG / QIN JINGYUAN | European Patent Office | 2024

    Free access

    Wire harness radiating pipe sleeve

    ZHOU JIAN | European Patent Office | 2020

    Free access

    Movable heat radiating crossbeam

    DONG JIANGUO | European Patent Office | 2016

    Free access

    Battery charger heat radiating structure

    European Patent Office | 2018

    Free access