The invention discloses a propulsion system for a small high-orbit satellite public platform. The system comprises a plurality of thrusters arranged in the outer side of a satellite bottom plate cabin, and the thrusters comprise +Y and -Y direction electric thrusters respectively arranged in the outer side of the satellite bottom plate cabin and +X and -X direction chemical thrusters arranged in the outer side of the satellite bottom plate cabin.

    本发明公开一种用于小型高轨卫星公用平台的推进系统,包括布置于卫星底板舱外侧的若干个推力器,其中,所述推力器包括分别设置于卫星底板舱外侧的+Y及‑Y向的电推力器以及设置于卫星底板舱外侧的+X及‑X向化学推力器。


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    Titel :

    Propulsion system for small high-orbit satellite public platform


    Weitere Titelangaben:

    一种用于小型高轨卫星公用平台的推进系统


    Beteiligte:
    JIANG GUOWEI (Autor:in) / LIN BAOJUN (Autor:in) / SHEN YUAN (Autor:in) / CHEN ZHICHAO (Autor:in) / CAO XIN (Autor:in)

    Erscheinungsdatum :

    27.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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