Basic principles and assumptions in calculating rocket combustion characteristics; outline of method commonly accepted for determining theoretical performance of rocket motors with different propellants; computed results for various propellant combinations are given and discussed. Based on Chapter IV of author's forthcoming book, "Rocket Propulsion Elements".


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    Title :

    Thermochemistry of rocket propellants


    Additional title:

    Am Rocket Soc -- J


    Contributors:

    Published in:

    Publication date :

    1947


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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