The invention relates to an all-electric propulsion satellite platform configuration, and belongs to the field of satellite platform design. The electric propulsion module is mounted on the side wall of the satellite body module; the solar wing module is installed on the side wall of the satellite body module, and the solar wing module and the electric propulsion module are located on the same side wall of the satellite body module. The expansion type heat radiator module is installed on the side wall of the satellite body module. The antenna module is mounted at the top of the satellite body module and the upper parts of the two side walls; the satellite-rocket docking module is mounted at the bottom of the satellite body module; the satellite-rocket docking module connects a satellite and a carrier rocket together and reliably separates the satellite and the carrier rocket in a satellite-rocket separation stage; the compact type flat satellite body structure is adopted, the efficient ion electric propulsion system, the high-storage-ratio winding type solar wing and the efficient thermal control system are configured, the launching cost is reduced, and the overall performance such as the weight, the power and the heat dissipation of the effective load borne by the full-electric propulsion satellite can be greatly improved.

    本发明涉及一种全电推进卫星平台构型,属于卫星平台设计领域;电推进模块安装在星本体模块的侧壁上;太阳翼模块安装在星本体模块的侧壁上,且太阳翼模块与电推进模块位于星本体模块相同的侧壁;展开式热辐射器模块安装在星本体模块的侧壁上;天线模块安装在星本体模块的顶部及2个侧壁的上部;星箭对接模块安装在星本体模块的底部;星箭对接模块将卫星与运载火箭连接在一起,并在星箭分离阶段将两者可靠分离;本发明采用紧凑型扁平式星本体构型,并配置了高效离子电推进系统、高收纳比卷绕式太阳翼、高效热控系统,降低发射成本,并可大幅提升全电推卫星承载有效载荷的重量、功率、散热等总体性能。


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    Title :

    All-electric propulsion satellite platform configuration


    Additional title:

    一种全电推进卫星平台构型


    Contributors:
    LI ZHENGJU (author) / WANG XINGLONG (author) / CAI YAXING (author) / LYU HONGJIAN (author) / WANG MIN (author) / YAO YUAN (author) / XU HONGYAN (author) / ZHANG HE (author) / TAO CHENG (author) / ZOU SHUANG (author)

    Publication date :

    2024-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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