우주발사체 추진기관의 신뢰도 평가

Evaluation of reliability for propulsion system of launch vehicle

  • 조상연 (한국항공우주연구원 추진기관그룹) ;
  • 김용욱 (한국항공우주연구원 추진기관그룹) ;
  • 오승협 (한국항공우주연구원 추진기관그룹) ;
  • 박찬빈 (한국항공우주연구원 기술경영그룹)
  • Cho, S.Y. (Propulsion system department, Korea Aerospace Research Institute) ;
  • Kim, Y.W. (Propulsion system department, Korea Aerospace Research Institute) ;
  • Oh, S.H. (Propulsion system department, Korea Aerospace Research Institute) ;
  • Park, C.B. (System engineering management Department, Korea Aerospace Research Institute)
  • 발행 : 2005.01.31

초록

In executing the large scale national project, such as development of space launch vehicle, it is most important to guarantee the technological reliability. However the reliability analysis of launch vehicle is different from other mass product goods because of the limitation of budget and number of tests. In this study, the reliability analysis technique of the propulsion system, which is one of the major sub-systems of launch vehicle is illustrated and applied to the liquid rocket engine of KSR-III.

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