Propulsion unit of 17 in. diam was developed by CARDE, Canadian Armament Research and Development Establishment for high altitude research vehicle; "CARDEPLEX" propellant used in motor is aluminized ammonium perchlorate/polyurethane formulation; axial combustion instability was factor which dictated pace of motor development; experimental investigations led to method of tailoring propellant compositions to obtain optimum combustion stability characteristics at prescribed burning rates; method was used in selection of propellant for 23KS20000 motor.
Development of 23KS20000 motor for Black Brant IIB vehicle
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 11 , n 10
1965
7 pages
Article (Journal)
English
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MOTOR DEVELOPMENT FOR THE BLACK BRANT VB
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