TVC(Thrust Vector Control) Actuator System for Liquid Engine |
Lee, Hee-Joong
(한국항공우주연구원)
Park, Moon-Su (한국항공우주연구원) Min, Byeong-Joo (한국항공우주연구원) Roh, Woong-Rae (한국항공우주연구원) Choi, Hyung-Don (한국항공우주연구원) |
1 | 민병주, 박문수, 이희중, 최형돈, "3단형 과학로켓 김발엔진 구동장치 개발," 한국항공우주학회지, 제30권, 제6호, 2002, pp. 116-123. |
2 | Kohno, M., Kawaguchi, J., Asai, T., Onojima, N., and Okaya, S. "Conceptual Study of the Movable Nozzle TVC System or M-V Launch Vehicle," 17th International ymposium on Space Technology and Science, Tokyo, Japan, 1990, pp.243-248. |
3 | Morita, Y., Kohno, M., Matsuo, H., Okaya, S., and Maruizumi, H., "On the M-V Attitude Control System, Part II: Hardware Design," 18th International Symposium on Space Technology and Science, Kagoshima, Japan, 1992, pp.985-990. |
4 | John F. Blackburn, Fluid Power Control, The MIT Press, 1960. |
5 | Liquid Rocket Actuators and Operators, NASA-SP-8090. |
6 | William A. Neese, Aircraft Hydraulic System, Krieger Publishing Company, 1991. |
7 | Herbert E. Merritt, Hydraulic Control Systems, John Wiley & Sons, 1967. |
8 | Benjamin C. Kuo, Automatic Control Systems, Prentice-Hall, 1991. |