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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    Titel :

    Rocket take-off method


    Weitere Titelangaben:

    一种火箭起飞方法


    Beteiligte:
    JIA JIEFENG (Autor:in)

    Erscheinungsdatum :

    03.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



    Rocket-assisted take-off

    Bailey-Watson, C.B. | Engineering Index Backfile | 1945


    Rocket-assisted take-offs

    Krzywoblocki, Z. | Engineering Index Backfile | 1946


    Rocket-assisted take-off for Buccaneer

    Engineering Index Backfile | 1965



    Small rocket take-off stability augmentation platform

    CAO JIANBAO | Europäisches Patentamt | 2020

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