The present invention relates to a flight thrust production method, wherein a thrust plate is arranged in the front of an injection nozzle injecting high-pressure gas generated by igniting fuel in a flight vehicle to the outside of the flight vehicle, and the injected high-pressure gas collides with the thrust plate to generate thrust. Moreover, gas having collided with the thrust plate is injected to the outside with a booster nozzle to generate reaction thrust. Therefore, efficiency of energy utilization can be increased.

    본 발명은 비행체 내부에서 연료를 발화 발생 되는 고압의 가스를 비행체 외부로 분사하는 분사노즐 전면에 추력판을 배치 분사되는 고압가스를 충돌시켜 추력을 발생시키고, 추력판에 충돌된 가스를 부스터노즐을 이용 외부로 분사 반작용 추력을 발생시키는 것으로 에너지이용 효율을 높은 비행추력 생산 방법에 관한 것이다.


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    Titel :

    Flight thrust production method


    Weitere Titelangaben:

    비행추력 생산 방법


    Beteiligte:
    LEE CHUNG HUEN (Autor:in)

    Erscheinungsdatum :

    11.05.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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