The invention discloses a double-Z-shaped 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, an intercepting rope is connected between the tractors on every two guide rails which are oppositely arranged, and the intercepting ropes are connected with the guide rails. And the two ends of the interception cable respectively bypass the pulleys of the two tractors and then are connected with the mass blocks below the two platforms which are oppositely arranged. According to the double-Z-shaped rocket capturing system, the requirements for the posture and speed of rocket recovery can be lowered, and the success rate of rocket recovery is increased.

    本发明公开了一种双Z字型火箭捕捉系统,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质量块连接。其目的是为了提供一种双Z字型火箭捕捉系统,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。


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    Title :

    Double-Z-shaped rocket capturing system


    Additional title:

    一种双Z字型火箭捕捉系统


    Contributors:
    YANG WEIJIE (author) / LI DINGSHI (author) / XU XUELEI (author) / WANG HUAJI (author) / ZHANG ZHI (author) / XU HONGPING (author) / ZHANG XIAO (author) / ZHANG HAILIAN (author) / WU RUNSHENG (author) / WU MENGQIANG (author)

    Publication date :

    2024-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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