The invention discloses a space flying net launching device and method. The device comprises an outer cylinder, an inner cylinder and a space flying net. The outer cylinder is provided with a first cavity and a first launching port, and the inner cylinder is detachably arranged in the first cavity through an inner cylinder launching mechanism; and the inner cylinder is provided with a second cavity and a second launching opening, the space flying net is contained in the second cavity, and the inner cylinder is provided with a flying net launching mechanism connected with the space flying net. By means of the two-stage launching mode, the defect that a traditional ejection mode cannot give consideration to the launching distance and the effective time is overcome, decoupling of two indexes is achieved, the launching distance and the effective time are both improved, and the performance of the flying net capturing device is improved; and secondly, since the two-stage emission mode realizes decoupling of the emission distance and the effective time, the parameters can be respectively considered and adjusted to change the emission distance and adjust the second-stage emission parameter to change the effective time during parameter design, and the efficiency of design work is improved.
本发明公开一种空间飞网发射装置及方法,该装置包括外筒体、内筒体与空间飞网;外筒体上设有第一腔体与第一发射口,内筒体通过内筒发射机构可拆卸的设在第一腔体内;内筒体上设有第二腔体与第二发射口,空间飞网收纳在第二腔体内,内筒体上设有与空间飞网相连的飞网发射机构。通过两级发射模式,消除了传统弹射模式不能兼顾发射距离和有效时间的弊端,实现了两个指标的解耦,使得发射距离和有效时间均得到了提高,提高了飞网捕获装置的性能;其次,由于两级发射模式实现了发射距离和有效时间的解耦,在参数设计时可以分别进行考虑,调整第一级发射参数以改变发射距离,调整第二级发射参数以改变有效时间,提高了设计工作的效率。
Space flying net launching device and launching method
一种空间飞网发射装置及发射方法
2021-06-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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