A mathematical model of hybrid combustion regression is derived which rationally encompasses the chemical kinetic and gasdynamic factors. Data from Smoot and Price (AIAA J. v3 p1408 1965) are used to confirm the resulting regression rate equation.


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    Title :

    Hybrid Rocket Combustion Regression Rate Model


    Contributors:
    E. Miller (author)

    Publication date :

    1966


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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