The invention aims to provide a satellite, a satellite module assembly and a satellite module connecting unit. The satellite module connecting unit comprises a first seat body, a second seat body and a connecting assembly. The connecting assembly is arranged in the connecting surface of the first seat body and/or the second seat body; the connecting assembly comprises a magnetic attraction module, a power supply module and a communication module; the plurality of connecting rods are connected between the first seat body and the second seat body. Wherein the two ends of each connecting rod are hinged to the first seat body and the second seat body respectively, each connecting rod is configured to be telescopic, and the posture of the first seat body relative to the second seat body can be adjusted by adjusting the length of one or more connecting rods in a telescopic mode, so that the satellite can meet the space mission scene with the high posture precision requirement.

    本发明的目的在于提供一种卫星、卫星模块组件及卫星模块连接单元,其中卫星模块连接单元包括第一座体、第二座体以及连接组件。连接组件设置于第一座体和/或第二座体连接面中,连接组件包括磁吸模块、供电模块以及通信模块。多个连接杆连接于第一座体与第二座体之间。其中,每个连接杆的两端分别与第一座体以及第二座体铰接,且每个连接杆均配置为可伸缩,通过伸缩调节一个或多个连接杆的长度,能够调节第一座体相对第二座体的姿态,以能够使得卫星可满足姿态精度要求高的太空任务场景。


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    Title :

    Satellite, satellite module assembly and satellite module connection unit


    Additional title:

    卫星、卫星模块组件及卫星模块连接单元


    Contributors:
    GUO CHONGBIN (author) / DU YANG (author) / YIN ZENGSHAN (author) / ZHANG JUN (author)

    Publication date :

    2023-04-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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