A device for the recovery of a proportion of the energy which is dissipated, by the Joule effect, by the equipment of a predetermined satellite in a vacuum atmosphere, includes at least one radiative panel (10) which is designed to permit the cooling of the satellite (20) payload, and a thermoelectric generator, the heat source (12) of which is supplied with infrared photons by the radiative panels (10), whereby the latter are configured to concentrate the infrared photons towards the heat source (12).


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    Title :

    Dispositif de récupération d'énergie thermique dissipée par un satellite placé dans le vide


    Additional title:

    Device for recovering thermal energy dissipated by a satellite placed in a vacuum
    Vorrichtung zur Rückgewinnung von Wärmeenergie, die von einem im Vakuum befindlichen Satelliten abgegeben wird


    Contributors:

    Publication date :

    2017-12-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H10N