A radiative fin for a spacecraft is disclosed having an end fitting of heat conductive material, configured to be mounted on the spacecraft, a flexible radiative laminate, connected to the end fitting at one end and having an opposite free end, at least one pyrolytic graphite sheet, and at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and a flexible rod, extending from the end fitting along at least part of a side of the flexible radiative laminate and being affixed to the latter. The flexible rod is adapted to occupy a folded position and a deployed position and to exert, while in the folded position, a deployment torque adapted to bring the flexible rod back to the deployed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FLEXIBLE RADIATIVE FIN FOR A SPACECRAFT


    Beteiligte:
    MENA FABRICE (Autor:in) / BENTHEM BRUIN (Autor:in)

    Erscheinungsdatum :

    23.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Flexible radiative fin for a spacecraft

    MENA FABRICE / BENTHEM BRUIN | Europäisches Patentamt | 2022

    Freier Zugriff

    A FLEXIBLE RADIATIVE FIN FOR A SPACECRAFT

    MENA FABRICE / BENTHEM BRUIN | Europäisches Patentamt | 2021

    Freier Zugriff

    A FLEXIBLE RADIATIVE FIN FOR A SPACECRAFT

    MENA FABRICE / BENTHEM BRUIN | Europäisches Patentamt | 2022

    Freier Zugriff

    Radiative cooler for spacecraft

    Mccullough, J. E. | NTRS | 1972


    Radiative Cooling Panels For Spacecraft

    LIU VICTOR / CASSE BERNARD D / DANIEL GEORGE et al. | Europäisches Patentamt | 2017

    Freier Zugriff