Twenty-eight inch, 700 lb, fiberglass encased rocket engine having capability of putting 200 lb payload into 300 nautical mi circular orbit is described; performance and environmental requirements; design, case manufacture, insulation, nozzle, and propellant are discussed.


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    Title :

    Solid propellent motor for third stage of satellite launcher


    Additional title:

    Spaceflight


    Contributors:
    Darwell, H.M. (author) / Raine, P.S. (author)

    Published in:

    Spaceflight ; 9 , n 4


    Publication date :

    1967


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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