Flexible Exit Cone Nozzle Demonstration Firing Results
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
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This report describes the test firing of a thrust vector control system TVC on the AFRPL 40-inch-diameter Char Motor. The TVC system consisted of a movable exit cone Flex-X nozzle and support hardware, which was designed to combine the advantages of the elastomeric seal with those of the supersonic split-line nozzle.
- Solid Propellant Rocket Engines