The invention discloses an I-shaped rocket recovery system which comprises four recovery platforms, a sliding rail is arranged between every two adjacent recovery platforms, the four recovery platforms and the four sliding rails are arranged in a rectangular shape, a pulley is arranged on each sliding rail in a sliding mode, an arresting cable is connected between the pulleys on every two oppositely-arranged sliding rails, and the recovery platforms are arranged on the recovery platforms. A traction device is installed between every two adjacent recycling platforms, and the traction devices can pull the tackles between the two adjacent recycling platforms to slide along the sliding rails. According to the I-shaped rocket recovery system, the requirements for the attitude and speed of rocket recovery can be lowered, and the success rate of rocket recovery is increased.

    本发明公开了一种工字型火箭回收系统,其包括四个回收平台,相邻两个回收平台之间设有滑轨,四个回收平台和四个滑轨呈矩形布置,每个滑轨上都滑动设有滑车,相对布置的两个滑轨上的滑车之间连接有阻拦索,相邻两个回收平台之间安装有牵引装置,牵引装置能够拉动该相邻两个回收平台之间的滑车沿着滑轨滑动。其目的是为了提供一种工字型火箭回收系统,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 :

    I-shaped rocket recovery system


    Additional title:

    一种工字型火箭回收系统


    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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