Investigation for particular case of hydrogen gas flowing adiabetically through typical rocket nozzle having chamber to throat area ratio of 2 to 1.


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    Title :

    Chemical kinetics and rocket nozzle design


    Additional title:

    Am Rocket Soc -- J


    Contributors:

    Published in:

    Publication date :

    1951


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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