The invention relates to a satellite separation device, and belongs to the field of satellite launching. Comprising a separation box shell, a separation mechanism, a launching mechanism, a transmission mechanism and a satellite storage box, the separation mechanism is arranged above the launching mechanism, the transmission mechanism is arranged on the side edges of the separation mechanism and the launching mechanism, the transmission mechanism is connected with the separation mechanism and the launching mechanism, and the transmission mechanism is connected with the transmission mechanism. The separation mechanism, the launching mechanism and the transmission mechanism are all arranged in the separation box shell, and the satellite storage box is installed on the outer side wall of the separation box shell. According to the invention, the launching speed and quantity of a plurality of miniature cubesas can be adjusted.

    本发明涉及一种卫星分离装置,属于卫星发射领域。包括:分离箱外壳、分离机构、发射机构、传动机构和卫星储存箱,所述分离机构设置在所述发射机构上方,所述传动机构设置在所述分离机构和所述发射机构的侧边,所述传动机构与所述分离机构和所述发射机构连接,所述分离机构、所述发射机构和所述传动机构均设置在所述分离箱外壳内部,所述卫星储存箱安装在所述分离箱外壳外侧壁上。本发明有利于对多个微型立方体卫星的发射速度和数量进行调整。


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    Title :

    Satellite separation device


    Additional title:

    一种卫星分离装置


    Contributors:
    ZHANG RUIBIN (author) / WANG RUI (author) / JIANG CHUNYAN (author) / HUANG XIANGLI (author) / CHEN RUI (author) / MO XINLIANG (author)

    Publication date :

    2023-07-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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