References
- Blaine W. Andersen, "The Analysis and Desing of Pneumatic Systems", Robert E. Krieger Publishing Company, 1976.
- 손병진 외, "유압공학", 탑출판사.
- 강춘길 외, "공압식 미익전개장치 개발보고서", 국방과학연구소, ADDR-S416-09079, 2009.
The fins of a missile which is folded within a canister are deployed according to a command during the missile flight. The aerodynamic load generated by operating environments such as missile flight speed, platform movement speed and wind acts as an anti-deploying force and prevents the fins from deploying. As the diversification of platforms and the higher speed of missiles need a larger deploying force but the space for operating the fin deploying device is getting narrower, the new design concepts are required for developing such a device. In this study, a pneumatic device for deploying missile fins is designed and its characteristics are verified through experiments and analyses.