Optimum staging principles for determining relative weights of stages of solid propellant rocket vehicle are established and relative influence of specific impulse and propellant mass fraction of various stages on performance of optimized multistage system investigated.


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    Title :

    Optimum staging of solid-propellant rocket vehicles


    Additional title:

    Astronautica Acta


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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