고기동 추력기 밸브 구동용 날개연동형 전기식 구동기 개발

A valve"s high response for controlling thruster is essential for rapid turning during initial short moment after launching. The actuator for controlling the valve is simultaneously used in controlling canard of a guided missile. This paper explain development process for the electromechanical actuator interlocked with canard by arranging in following order, design, analysis, manufacture, test and evaluation.