The field of hybrid propulsion marked 2015 with several notable accomplishments, global collaborations and geographical expansions. Here, Majdalani discusses these accomplishments, collaborations and expansions. Researchers at the Japan Aerospace Exploration Agency simulated a hybrid design that utilizes an altering-intensity, swirl-oxidizer type flow. This design enhances performance through continuous thrust-independent control of the oxidizer-fuel ratio.


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    Title :

    Expanding the global footprint of hybrid rocketry


    Contributors:

    Published in:

    Publication date :

    2015



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.88 Luftverkehr, Raumfahrt / 55.88
    Local classification TIB:    770/7040



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