The invention provides a rocket fairing recovery system and method, and belongs to the technical field of rocket sublevel recovery. The rocket fairing recovery system provided by the invention comprises a deceleration system, a control system and an aerial grabbing system, wherein the deceleration system comprises a controllable parafoil and a thrust reverser which are arranged on a fairing; the control system is used for controlling operation of the controllable parafoil and the thrust reverser; and the aerial grabbing system comprises an air vehicle which is provided with a mechanical arm for conducting aerial grabbing on the fairing. According to the rocket fairing recovery system, the fairing grabbed in the air does not need to be received on the ground, the aerial grabbing mode has better maneuverability compared with other receiving modes, safe landing of the fairing can be ensured, and secondary use of the fairing is ensured.

    本发明提供的一种火箭整流罩回收系统及方法,属于火箭子级回收技术领域,本发明提供的火箭整流罩回收系统,包括:减速系统,包括设置在整流罩上的可控翼伞和反推装置;控制系统,用于控制所述可控翼伞和反推装置的运行;空中抓取系统,包括飞行器,所述飞行器具有用于对整流罩实施空中抓取的机械臂;本发明的火箭整流罩回收系统中,在空中对整流罩的抓取,无需再在地面进行接收,空中的抓取相对于其他的接收方式有更好的机动性,能够保证整流罩的安全着落,保证整流罩的二次使用。


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    Titel :

    Rocket fairing recovery system and method


    Weitere Titelangaben:

    火箭整流罩回收系统及方法


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

    Erscheinungsdatum :

    2020-05-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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