This report discusses the design, analysis, and performance evaluation of a helium driven closed center servo actuator system. The actuator was sized to operate a trapped ball type of movable nozzle thrust vector control system for tactical missiles. Predicted and actual performance are compared and typical test data are presented. (Author)
Low Cost Servo Actuator for Tactical Missile Thrust Vector Control (TVC)
1977
118 pages
Report
No indication
English
Optimal thrust vector control of tactical missiles
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