A radiator for a geostationary satellite is disclosed having a radiative panel perpendicular to a radiation axis, and pivoting relative to the radiation axis, a mounting foot for the panel, a motor which rotates the mounting foot about a rotation axis, the radiation axis and the rotation axis being tilted relative to each other by an angle corresponding to the angle of the satellite's orbital plane relative to the ecliptic plane of the planet, and a guidance system for the panel, limiting rotation of the panel about the rotation axis, including a connecting arm pivoting relative to the satellite about a first axis and relative to the panel about a second axis concurrent with the first axis at a point of intersection of all the axes.


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    Title :

    SATELLITE GÉOSTATIONNAIRE COMPRENANT UN RADIATEUR À ENSOLEILLEMENT RÉDUIT ET SYSTÈME DE GUIDAGE AMÉLIORÉ


    Additional title:

    GEOSTATIONARY SATELLITE COMPRISING A RADIATOR WITH REDUCED INSOLATION AND IMPROVED GUIDANCE SYSTEM
    GEOSTATIONÄRER SATELLIT UMFASSEND EINEN STRAHLER MIT VERMINDERTER SONNENEINSTRAHLUNG UND VERBESSERTEM FÜHRUNGSSYSTEM


    Contributors:

    Publication date :

    2023-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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