The invention provides a rocket takeoff method which is applied to a rocket takeoff stage, and compared with an existing takeoff process, the method does not need working processes such as propellant replenishing, engine pre-cooling and pressurized gas replenishing.

    本发明提供了一种火箭起飞方法,该方法应用在火箭起飞阶段,相比现有起飞流程,该方法不需要推进剂补加、发动机预冷、增压气体补加等工作流程。


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    Title :

    Rocket take-off method


    Additional title:

    一种火箭起飞方法


    Contributors:
    JIA JIEFENG (author)

    Publication date :

    2024-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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