Theory indicates that certain combinations of propellants have greater propulsive capability than either propellant alone; optimum performance results from suitably programmed variation of propellant proportions throughout burning; results applicable to first stage of rocket presented.


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    Title :

    Optimum proportioning of two propellants to obtain maximum burnt velocity


    Additional title:

    ARS -- J


    Contributors:
    Olds, R.H. (author)

    Published in:

    ARS Journal ; 29 , n 8


    Publication date :

    1959


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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