A satellite deorbiting device including an aerobraking surface including a satellite attitude control device with gravity gradient, the device with gravity gradient including at least one mast carrying the aerobraking surface, a first end of which is secured to the satellite and the second end of which is provided with a mass, such that the mast is oriented in a direction opposing that of the planet around which the satellite orbits.


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    Title :

    СИСТЕМА АЭРОДИНАМИЧЕСКОГО ТОРМОЖЕНИЯ ДЛЯ СХОДА СПУТНИКА С ОРБИТЫ


    Publication date :

    2019-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS