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액체엔진 추력벡터제어 구동장치시스템

TVC(Thrust Vector Control) Actuator System for Liquid Engine

  • 발행 : 2004.06.01

초록

키워드

참고문헌

  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. William A. Neese, Aircraft Hydraulic System, Krieger Publishing Company, 1991.
  5. Benjamin C. Kuo, Automatic Control Systems, Prentice-Hall, 1991.
  6. Herbert E. Merritt, Hydraulic Control Systems, John Wiley & Sons, 1967.
  7. John F. Blackburn, Fluid Power Control, The MIT Press, 1960.
  8. Liquid Rocket Actuators and Operators, NASA-SP-8090.