A simplified self-consistent method for the study of high-acceleration solid-propellant rockets was developed. 'High acceleration' means values of acceleration approaching the theoretical upper limit. This limit is determined primarily by the structural material strength and density, the payload, the stage burnout velocity, and the weight burning rate and specific impulse of the available propellant.


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    Title :

    The Preliminary Design of High-Acceleration Solid-Propellant Rockets


    Contributors:
    R. H. Fox (author)

    Publication date :

    1964


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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