A cryogenic engine for a space apparatus is provided. The cryogenic engine includes an injector body, a thrust chamber, and a spark plug, where the injector body is provided therein with an accommodating space; the spark plug is provided on one side of the injector body, and an electrode provided on the spark plug extends into the accommodating space; the thrust chamber is provided on the other side of the injector body and is communicated with the accommodating space; the injector body is provided with a combustion improver flow channel and a combustible agent flow channel; and the combustion improver flow channel and combustible agent flow channel are connected with the accommodating space.


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    Titel :

    CRYOGENIC ENGINE FOR SPACE APPARATUS


    Beteiligte:
    CHENG CHENG (Autor:in) / ZHOU HAIQING (Autor:in) / TIAN GUI (Autor:in) / XIONG JINGYU (Autor:in) / ZENG YEMING (Autor:in) / ZHOU GUOFENG (Autor:in) / XU HONGBO (Autor:in)

    Erscheinungsdatum :

    2023-10-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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