The invention relates to an on-orbit service module based on a ground testing interface and belongs to the technical field of on-orbit service of spacecrafts. The on-orbit service module comprises a satellite-rocket separating plug X1F, a power supply processing unit PPU, a thruster switching unit, a north side ion thruster, a south side ion thruster, an integrated electronic processing unit IEPCP, a pressure regulating module, a flow control module, a vector adjusting mechanism, a thermal control unit and an abutting mechanism. The on-orbit service module is abutted to a satellite-rocket separating plug X1F of an external served satellite through the satellite-rocket separating plug X1F. The invention provides a design thought of changing a unidirectional service relationship of a conventional service and a served object to achieve energy, measurement and control, control and propel sharing and interaction between the conventional service and the served object.

    本发明涉及一种基于地面测试接口的在轨服务模块,属于航天器在轨服务技术领域;包括星箭分离插头X1F、电源处理单元PPU、推力器切换单元、北侧离子推力器、南侧离子推力器、综电处理单元IEPCP、压力调节模块、流量控制模块、矢量调节机构、热控单元、对接机构;轨服务模块通过星箭分离插头X1F与外部被服务卫星的星箭分离插头X1F对接;本发明提出了改变传统服务与被服务对象的单向服务关系,实现两者能源、测控、控制、推进共享交互的设计思想。


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    Title :

    On-orbit service module based on ground testing interface


    Additional title:

    一种基于地面测试接口的在轨服务模块


    Contributors:
    AN RAN (author) / HAN HUAN (author) / ZHANG XIAOMING (author) / YAN SENHAO (author) / DUAN CHUANHUI (author) / REN LIXIN (author)

    Publication date :

    2020-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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