The invention provides a rocket substage landing recovery system and method, and belongs to the technical field of carrier rockets. The rocket substage landing recovery system comprises: a controllable propulsion deceleration system which is arranged on a rocket substage and is provided with a controllable propulsion engine for controlling the rocket substage to decelerate; a parachute system which comprises a parachute arranged in the interstage section of the rocket substage; a control system which is used for controlling the flight and attitude of the rocket substage; grid wings which are arranged on the rocket substages and are controlled by the control system; and a landing receiving system which is provided with a mobile landing platform used for receiving the rocket substages, wherein the mobile landing platform is provided with a landing buffer mechanism. According to the rocket substage landing recovery system, when the rocket substage cannot accurately land on the fixed landing platform, the rocket substage is controlled to be matched with the landing receiving system, and the rocket substage stably lands on the landing buffer mechanism.

    本发明提供的火箭子级着陆回收系统及方法,属于运载火箭技术领域,所述火箭子级着陆回收系统,包括:可控推进减速系统,设置在火箭子级上,具有用于控制所述火箭子级进行减速的可控推进发动机;降落伞系统,包括设置在火箭子级的级间段内的降落伞;控制系统,用于控制火箭子级的飞行和姿态;栅格翼,设置在火箭子级上,由所述控制系统控制;着陆接收系统,具有用于接收所述火箭子级的移动着陆平台,所述移动着陆平台上具有着陆缓冲机构;本发明的火箭子级着陆回收系统,当出现火箭子级不能准确的着陆在固定着陆平台上,控制火箭子级和着陆接收系统相配合,实现火箭子级平稳降落到着陆缓冲机构上。


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    Titel :

    Rocket substage landing recovery system and method


    Weitere Titelangaben:

    火箭子级着陆回收系统及方法


    Beteiligte:
    PENG XIAOBO (Autor:in) / ZHENG LIWEI (Autor:in) / SHI FASHU (Autor:in)

    Erscheinungsdatum :

    2020-06-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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