The invention provides a thermal isolation point type separation device satellite-rocket electric lap joint structure which comprises a satellite platform bottom plate, satellite-rocket separation device adapters and a satellite support, the satellite platform bottom plate is connected with the satellite support in a fastened mode through the multiple satellite-rocket separation device adapters, any satellite-rocket separation device adapter is connected with the satellite platform bottom plate in a fastened mode, and the satellite-rocket separation device adapter is connected with the satellite support in a fastened mode. A plurality of flat gaskets and elastic gaskets are arranged on the sides, close to the satellite platform bottom plate, of the satellite-rocket separation device adapters, a plurality of explosive bolts are correspondingly installed on the satellite support, and any satellite-rocket separation device adapter is connected with the satellite support in a fastened mode through the explosive bolts. After the point-type satellite-rocket separation device is connected with the satellite, the heat insulation requirement between the point-type satellite-rocket separation device and the satellite is guaranteed through the polyimide heat insulation pad, the electric lap joint performance is provided for the satellite and the rocket through the surface treatment state and the connection mode of the satellite-rocket separation device adapter, the structure is simple, installation and adjustment are convenient, and use is safe and reliable.

    本发明提供了一种热隔离的点式分离装置星箭电搭接结构,包括卫星平台底板、星箭分离装置转接件以及卫星支架,卫星平台底板通过多个星箭分离装置转接件与卫星支架紧固连接,任一星箭分离装置转接件均与卫星平台底板紧固连接,且星箭分离装置转接件靠近卫星平台底板的一侧设置有多个平垫和弹垫,卫星支架上对应安装有多个爆炸螺栓,任一星箭分离装置转接件均通过爆炸螺栓与卫星支架紧固连接。本发明在点式星箭分离装置与卫星连接后,通过聚酰亚胺隔热垫保证点式星箭分离装置与卫星之间的隔热要求,通过星箭分离装置转接件的表面处理状态和连接形式为星箭提供电搭接性能,结构简单、安装调整方便、使用安全可靠。


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    Title :

    Thermal isolation point type separation device satellite-rocket electric lap joint structure


    Additional title:

    热隔离的点式分离装置星箭电搭接结构


    Contributors:
    CHEN TING (author) / CHEN GUOZHONG (author) / CHEN YUNLI (author) / HUANG WEIDONG (author) / XU SHENXIN (author)

    Publication date :

    2024-10-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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