The invention discloses an orbit control detonation power device and an aircraft. The orbit control detonation power device comprises an outer shell, an oxidizing agent storage tank, a fuel oil storage tank and a detonation engine, wherein the oxidizing agent storage tank, the fuel oil storage tank and the detonation engine are contained in the outer shell. And the oxidant storage tank and the fuel storage tank are respectively connected with the detonation engine through pipelines.

    一种轨控爆震动力装置及飞行器,轨控爆震动力装置包括外壳体、收容于所述外壳体内的氧化剂储存罐、燃油储存罐、及爆震发动机;所述氧化剂储存罐、燃油储存罐通过管路分别与所述爆震发动机连接。


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    Titel :

    Engine and combustion chamber structure thereof


    Weitere Titelangaben:

    一种发动机及其燃烧室结构


    Beteiligte:
    WEI HUANCHENG (Autor:in) / WANG LIN (Autor:in) / GAO ZONGYONG (Autor:in) / LYU BING (Autor:in)

    Erscheinungsdatum :

    13.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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