The invention provides a separating and releasing mechanism of stacked panel satellites and a carrier rocket. The separating and releasing mechanism comprises a pressing rod support suitable for being switched between a press-fit state and an unfolding state, in the press-fit state, the pressing rod support is suitable for being pressed on a first panel satellite on the uppermost layer of a satellite stacking column, and in the unfolding state, the pressing rod support leaves the position above the first panel satellite; the extension part is provided with a head end and a tail end which are opposite to each other, and an axial channel is formed in the extension part; the clamping jaw is exposed out of the tail end of the extending part and connected with the tail end of the extending part, the clamping jaw has an opening state and a closing state, and the normal state is the opening 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. The satellite separation time sequence can be controlled, and the collision risk is reduced.
本申请提供了一种堆叠平板卫星的分离释放机构及运载火箭。分离释放机构包括:压杆支架,适于在压合状态和展开状态间切换,在所述压合状态下,所述压杆支架适于压在卫星堆叠柱最上层的第一平板卫星上,在所述展开状态下,所述压杆支架离开所述第一平板卫星上方;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;卡爪,露出于所述延伸部末端且连接所述延伸部末端,所述卡爪具有张开状态和收拢状态,且常态为张开状态;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。本申请能够控制卫星分离时序,降低碰撞风险。
Separating and releasing mechanism of stacked panel satellites and carrier rocket
堆叠平板卫星的分离释放机构及运载火箭
2025-02-28
Patent
Electronic Resource
Chinese
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