Background and development program of high performance 10-in. diam, 125-in. long solid propellant rocket engine by Canadian Armament Research and Development Establishment (CARDE); several CARDEPLEX (polyurethane-ammonium perchlorate) propellants of approximately required burning rate were available for consideration; propellant choice and stability; ballistic design and engine layout; static testing of flight engine; performance.


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    Title :

    Development of 9KS11000 Black Brant III rocket engine


    Additional title:

    Can Aeronautics Space J


    Contributors:


    Publication date :

    1962


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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