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Low Cost Servo Actuator for Tactical Missile Thrust Vector Control (TVC)
Final rept. 22 Apr-19 Oct 1976
FORD AEROSPACE AND COMMUNICATIONS CORP NEWPORT BEACH CA AERONUTRONIC DIV
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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.
APPROVED FOR PUBLIC RELEASE