The invention discloses a tethered satellite ejection release mechanism, which belongs to the field of satellite release mechanisms, is high in modularization degree and has no influence on the design of satellites. The device comprises a release control mechanism and a child satellite, the release control mechanism and the child star are connected with the base through a main shaft and are locked through a pin puller mounted on the base; the mechanism is simple in structure, small in number of parts, light in weight and high in modularization degree; the mechanism can be used as an independent module of a satellite to work, and only the satellite needs to send an unlocking instruction and a motor control signal to the mechanism; the device can be used for catapult separation of the child satellites and release control of the child satellites.

    本发明公开了一种绳系卫星弹射释放机构,属于卫星释放机构领域,所述机构模块化程度高,且对卫星的设计不产生影响。本发明包括:释放控制机构、子星;所述释放控制机构与子星通过主轴与底座实现连接,并通过安装在底座上的拔销器进行锁定;本发明机构结构简单,零件数量少,重量轻,模块化程度高;可作为卫星的一个独立模块进行工作,只需要卫星对此机构发送解锁指令以及电机控制信号即可;能够用于子星的弹射分离以及对子星进行释放控制。


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    Title :

    Tethered satellite ejection release mechanism


    Additional title:

    一种绳系卫星弹射释放机构


    Contributors:
    CHEN TI (author) / LIAO ZHIFENG (author) / WANG JINGXU (author) / CHENG KEXIN (author) / PENG WENXUAN (author) / YUN WEIDONG (author) / LI DONGDONG (author)

    Publication date :

    2024-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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