The invention discloses a booster and core-level integral separated liquid carrier rocket. The liquid carrier rocket comprises a core level with at least one core level and at least one booster. In the whole process of final assembly, testing, filling and launching of the liquid carrier rocket, the booster is rigidly connected to the peripheral side of the one core level. The liquid carrier rocket has the characteristics that the flight reliability of the whole rocket is improved, and the structural weight and cost are reduced.

    本发明公开了一种助推器和芯级整体式分离的液体运载火箭,该液体运载火箭包括至少具有芯一级的芯级以及至少一个助推器;在液体运载火箭的总装、测试、加注以及发射全过程中,助推器均刚性连接于芯一级的外周侧。上述液体运载火箭具有提高全箭的飞行可靠性、降低结构重量和成本的特点。


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    Titel :

    Booster and core-level integral separated liquid carrier rocket


    Weitere Titelangaben:

    一种助推器和芯级整体式分离的液体运载火箭


    Beteiligte:
    ZHU XIONGFENG (Autor:in) / CHENG HONGWEI (Autor:in) / LIU YANG (Autor:in) / TAN YUNTAO (Autor:in) / YONG ZIHAO (Autor:in) / GU JIANGUANG (Autor:in) / LIU YING (Autor:in) / WANG YISHAN (Autor:in) / HAN QIULONG (Autor:in)

    Erscheinungsdatum :

    2021-06-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS





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