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Combination / separation method between satellite and rocket and apogee kick engine

机译:卫星与火箭的组合/分离方法及远地点反冲发动机

摘要

PURPOSE:To improve the reliability of the removal operation by combining a satellite, an apogee-kick engine, and a payload attaching fitting, with the same removing bolt, and combining the said engine and the satellite with a simple ratch mechanism. CONSTITUTION:In a composition in which an apogee-kick engine 2 is combined to a satellite 1, and a rocket 5 is combined to the satellite 1 through a payload attaching fitting 3, the flange at the satellite 1 side, the flange of the apogee- kick engine 2, and the flange of the payload attaching fitting 3 are fastened together with an explosion bolt 7 and a nut-form processed good 8 fixed to the payload attaching fitting 3, and they are connected each other. The explosion bolt 7 is held by a bolt catcher 9 when it is removed. And the flange at the satellite 1 side and the flange of the apposi-kick engine 2 are combined with a simple ratch mechanism to allow an easy removal.
机译:目的:通过将卫星,远地点踢引擎和有效载荷连接配件与相同的拆卸螺栓结合在一起,并通过简单的棘轮机构将所述发动机和卫星结合起来,以提高拆卸操作的可靠性。组成:在一种构型中,远地点踢发动机2与卫星1结合,火箭5通过有效载荷固定配件3与卫星1结合,卫星1侧的法兰即远地点的法兰-脚踏发动机2,利用固定在有效载荷安装配件3上的防爆螺栓7和螺母状加工品8将有效载荷安装配件3的凸缘紧固在一起。拆下时,爆炸螺栓7由螺栓捕捉器9固定。并且,将卫星1侧的凸缘和阿波西斯踢引擎2的凸缘与简单的棘轮机构结合在一起,从而易于拆卸。

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