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. (Author)
Flexible Exit Cone Nozzle Demonstration Firing Results
1969
23 pages
Report
Keine Angabe
Englisch
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