It is shown how performance has improved during past decade and how they can provide controlled thrust to meet any missile requirement; thrust control for solid propellant engines and three methods which would be applicable, namely, jet vanes, inclined tubular extension, and sliding beveled extension or ungulus; control of thrust magnitude.


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    Title :

    Future for solid propellant rockets


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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