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.
Development of 9KS11000 Black Brant III rocket engine
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 8 , n 6
1962
7 pages
Article (Journal)
English
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