The invention discloses a rocket capturing system which comprises four platforms, connecting lines among the four platforms are rectangular, a guide rail is arranged between every two adjacent platforms, a tractor is mounted on each guide rail, and an intercepting cable is connected between the tractors on every two guide rails which are oppositely arranged. And the two ends of the intercepting cable bypass the pulleys of the two tractors respectively and then are connected with the buffer mechanisms below the two platforms which are oppositely arranged. The invention aims to provide the rocket capturing system which can reduce the requirements on the attitude and speed of rocket recovery and improve the success rate of rocket recovery.
本发明公开了一种火箭捕捉系统,其包括四个平台,四个平台之间的连线呈矩形,相邻两个平台之间设有导轨,每根导轨上安装有牵引车,相对布置的两根导轨上的牵引车之间连接有拦截索,拦截索的两端分别绕过两个牵引车的滑轮后与相对布置的两个平台下方的缓冲机构连接。其目的是为了提供一种火箭捕捉系统,可以降低对火箭回收的姿态和速度要求,提高火箭回收的成功率。
Rocket capturing system
一种火箭捕捉系统
2024-05-03
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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