Flexible Exit Cone Nozzle Development Program.
Final rept. Aug 67-May 71,
THIOKOL CHEMICAL CORP BRIGHAM CITY UTAH WASATCH DIV
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This program was initiated by the Air Force Rocket Propulsion Laboratory to demonstrate the flexible exit cone omniaxis movable nozzle concept by rocket motor testing. Program objectives are as follows develop flexible exit cone design and criteria, perform a TVC system comparison, and demonstrate the flexible exit cone nozzle performance on four AFRPL 36 in. diameter char motor static tests with vectoring. Author
- Rocket Engines
- Solid Propellant Rocket Engines