The invention relates to the technical field of satellite generation, in particular to a large-batch satellite launching device and a separation method.The large-batch satellite launching device comprises a rocket launching tower which is of a cylindrical structure, multiple layers of satellite separation mechanisms are installed on the side face of the rocket launching tower in the axial direction of the rocket launching tower, and the multiple satellite separation mechanisms on each layer are evenly arranged in the circumferential direction of the rocket launching tower; the satellite separation mechanisms are connected with corresponding satellites, the satellites are separated and released through the satellite separation mechanisms, and meanwhile when the large-batch satellite separation method is operated, the rocket launching tower alternately controls the two satellite separation mechanisms symmetrically arranged at the two ends of the rocket launching tower, and the controller separates the correspondingly connected satellites. The problems that when an existing aviation launcher adopts a disordered separation mode to launch a large number of satellites, the overall attitude and mass gravity center changes of the satellites and rockets which are not separated are large, and attitude control and separation safety cannot be guaranteed are solved.
本发明涉及卫星发生技术领域,具体是一种大批量卫星发射装置以及分离方法,包括火箭发射塔,其为圆柱结构,所述火箭发射塔侧面沿其轴向方向安装有多层卫星分离机构,每层所述多组卫星分离机构沿火箭发射塔的周向均匀设置,所述卫星分离机构与对应卫星连接,由所述卫星分离机构对卫星进行分离释放,同时一种大批量卫星分离方法在操作时,所述火箭发射塔交替控制其两端对称设置的两组卫星分离机构,并控制器分离对应连接的卫星,解决了现有航空发射器采用无序分离模式在进行大批量卫星的发射时,未分离的卫星和火箭具整体姿态和质量重心变化大,无法保证姿控和分离安全的问题。
Large-batch satellite launching device and separation method
一种大批量卫星发射装置以及分离方法
2024-12-13
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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