The apparatus provides pitch, yaw and roll control for a rocket propelled missile. The propulsion system includes a thrust nozzle and a secondary injection thrust vector control system. A roll control capability is added to the secondary injection thrust vector control system. An arrangement is shown for deflecting the secondary jet by use of a tertiary injection system.
Tertiary Injector for Propulsion System Roll Control
1966
1 pages
Report
Keine Angabe
Englisch
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