The invention relates to the technical field of aerospace attitude and orbit control, in particular to a space centroid gas vane integrated power system and an aircraft, the space centroid gas vane integrated power system comprises an engine propulsion system, a centroid gas vane and a driving assembly, the engine propulsion system is arranged on a rack, and a spray pipe outlet of the engine propulsion system faces one side of a gas outlet in the rack; the fuel gas outlet is positioned at the mass center of the whole bomb; a plurality of centroid gas vanes are uniformly distributed in the gas outlet; the driving assembly is used for controlling the direction of the centroid gas vane so as to change the direction of gas sprayed by a spray pipe of the engine propulsion system, and on-orbit attitude control and orbital transfer control of the aircraft are carried out. According to the device, on-orbit attitude control and orbital transfer control of the aircraft are accurately realized.

    本发明涉及航天姿轨控制技术领域,具体涉及一种空间质心燃气舵一体化动力系统以及飞行器,包括:发动机推进系统、质心燃气舵以及驱动组件,发动机推进系统设置在机架上,且发动机推进系统的喷管出口朝向机架上燃气出口的一侧,且燃气出口位于全弹质心位置;多个质心燃气舵均布在燃气出口内;驱动组件用于控制质心燃气舵的方向,以改变发动机推进系统的喷管喷出气体的方向,进行飞行器的在轨姿控与变轨控制。本装置精确实现对飞行器的在轨姿控与变轨的控制。


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    Titel :

    Space centroid gas vane integrated power system and aircraft


    Weitere Titelangaben:

    空间质心燃气舵一体化动力系统以及飞行器


    Beteiligte:
    HUI AOBO (Autor:in) / LIU YANG (Autor:in)

    Erscheinungsdatum :

    23.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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