The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face. The satellite comprises a bearing structure carrying the North face, the South face, the East face and the West face. At least one part (54, 56) of said at least one main radiator (42, 44) protrudes from at least one face from the East face and the West face (36). The inner face of said at least one protruding part (54, 56) is covered with a high infrared emissivity material. The value of the dimension (L54,56) of said at least one protruding part (54, 56) is between 19% and 50% of the value of the distance (Lc) between the East and West faces.

    The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face The satellite comprises a bearing structure carrying the North face, the South face, the East face and the West face At least one part (54, 56) of said at least one main radiator (42, 44) protrudes from at least one face from the East face and the West face (36) The inner face of said at least one protruding part (54, 56) is covered with a high infrared emissivity material The value of the dimension (L54,56) of said at least one protruding part (54, 56) is between 19% and 50% of the value of the distance (Lc) between the East and West faces


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    Titel :

    SATELLITE ARTIFICIEL


    Weitere Titelangaben:

    ARTIFICIAL SATELLITE


    Beteiligte:
    CAEL PHILIPPE (Autor:in) / WALKER ANDREW (Autor:in) / MENA FABRICE (Autor:in)

    Erscheinungsdatum :

    08.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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