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조상연,김용욱,오승협,박찬빈,Cho, S.Y.,Kim, Y.W.,Oh, S.H.,Park, C.B. 한국시스템엔지니어링학회 2005 시스템엔지니어링학술지 Vol.1 No.1
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.