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
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Cameras on Black Brant II rocket
Engineering Index Backfile | 1968
|Black Brant IV LF/VLF Rocket Probe Experiment
NTIS | 1970
Cameras on a Black Brant II Rocket
NTIS | 1968
|