Review of development trends for solid propellant rockets of over 1, 000,000 lb thrust considers case and nozzle design and requirements for propellants, materials, and fabrication; partial tests, while yielding significant data, help conserve costly propellant and case material.


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    Title :

    Solids competitive for multi-million-pound boosters


    Additional title:

    Space/Aeronautics


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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