A first deployment mechanism (30) deploys a first radiator panel (20) from a state where the first radiator panel (20) is opposed to a north or south face (10) of the body structure of a satellite. A second radiator panel (40) is stacked with the first radiator panel (20) to be opposed to the north or south face (10) of the body structure of the satellite and is sandwiched between the north and south face (10) of the body structure of the satellite and the first radiator panel (20), in a state where the first radiator panel (20) is opposed to the north or south face (10) of the body structure of the satellite. A second deployment mechanism (50) connects the second radiator panel (40) to the north or south face (10) of the body structure of the satellite, and deploys the second radiator panel (40) in a direction P2 opposite to a deployment direction P1 of the first radiator panel from a state where the second radiator panel (40) is opposed to the north or south face (10) of the body structure of the satellite.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Deployable radiator


    Beteiligte:

    Erscheinungsdatum :

    08.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL



    DEPLOYABLE RADIATOR

    KAWAMURA SHUNICHI | Europäisches Patentamt | 2019

    Freier Zugriff

    Deployable radiator

    SHIN SO MIN / KIM SUNG JIN / KIM JU NO et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    DEPLOYABLE RADIATOR

    KAWAMURA SHUNICHI | Europäisches Patentamt | 2023

    Freier Zugriff

    DEPLOYABLE RADIATOR

    KAWAMURA SHUNICHI | Europäisches Patentamt | 2018

    Freier Zugriff

    Deployable heat-pipe radiator

    Edelstein, F. | NTRS | 1978