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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    Titel :

    Development of 9KS11000 Black Brant III rocket engine


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Roberts, A.K. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Cameras on Black Brant II rocket

    Wein, M. | Engineering Index Backfile | 1968




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