The invention provides a release mechanism of stacked panel satellites and a carrier rocket. The release structure comprises: an extension part having a head end and a tail end opposite to each other, the extension part having an axial channel inside; the inhaul cable is arranged in the channel in a penetrating mode, the inhaul cable is provided with a head end and a tail end which are opposite, and the tail end of the inhaul cable is close to the tail end of the extending part; the clamping jaw is exposed out of the tail end of the extending part and is connected with the tail end of the inhaul cable, and the normal state of the clamping jaw is an open state; the clamping jaw opening and closing assembly is connected with the head end of the inhaul cable and used for pulling back and releasing the inhaul cable so that the clamping jaw can be switched between the folded state and the unfolded state; and the extension part recycling assembly is connected with the head end of the extension part and used for driving the extension part to be recycled towards the rocket body of the rocket. According to the invention, the satellite-rocket/inter-satellite distance during release can be increased, and the collision risk is reduced.
提供一种堆叠平板卫星的释放机构及运载火箭。所述释放结构包括:延伸部,具有相对的头端和末端,所述延伸部内部具有沿轴向的通道;拉索,穿设于所述通道内,所述拉索具有相对的头端和末端,所述拉索末端靠近所述延伸部末端;卡爪,露出于所述延伸部末端且连接所述拉索末端,所述卡爪常态为张开状态;卡爪开合组件,连接所述拉索头端,用于回拉和释放所述拉索,使所述卡爪在收拢和张开状态间切换;以及延伸部回收组件,连接所述延伸部头端,用于带动所述延伸部向火箭的箭体方向回收。本申请能够增大释放时星箭/星间距离,降低碰撞风险。
Release mechanism of stacked panel satellites and carrier rocket
堆叠平板卫星的释放机构及运载火箭
2025-02-25
Patent
Electronic Resource
Chinese
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