Actuator System of Flexseal Bearing Movable Nozzle for Solid Motor

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고체모터 가동노즐 구동장치시스템

Andrew B. Facciano, Jet Vane Control System Prototype Hardware Development for the ESSM, Raytheon Missile System, 1998.
James R. Donat, "Solid Rocket Motor Nozzle Flexseal Design Sensitivity," AIAA/AHS/ASEE Aerospace Design Conference, Irvine, CA, USA, 1993.
민병주, 박문수, 이희중, 최형돈, "3단형 과학로켓 김발엔진 구동장치 개발," 한국항공우주학회지, 제30권, 제6호, 2002, pp.116-123.
Herbert E. Merritt, Hydraulic Control Systems, John Wiley & Sons, 1967.
Kohno, M., Kawaguchi, J., Asai, T., Onojima, N., and Okaya, S., "Conceptual Study of the Movable Nozzle TVC System for M-V Launch Vehicle," 17th International Symposium on Space Technology and Science, Tokyo, Japan, 1990, pp.243-248.
Morita, Y., Kohno, M., Matsuo, H., Okaya, S., and Maruizumi, H., "On theM-V Attitude Control System, Part II : Hardware Design," 18th International Symposium on Space Technology and Science, Kagoshima, Japan, 1992, pp.985-990.
Liquid Rocket Actuators and Operators, NASA-SP-8090.
Transient Loads from Thrust Excitation, NASA-SP-8030.
Benjamin C. Kuo, Automatic Control Systems, Prentice-Hall, 1991.