우주발사체 개발사업에서 신뢰성공학의 시스템엔지니어링 인터페이스

System Engineering Interfaces of Reliability Engineering in Development of Launch Vehicle

  • 신명호 (한국항공우주연구원 우주발사체사업단) ;
  • 조상연 (한국항공우주연구원 우주발사체사업단) ;
  • 조미옥 (한국항공우주연구원 우주발사체사업단)
  • Shin, Myoung Ho (KSLV Systems Devision, Korea Aerospace Research Institute) ;
  • Cho, Sang Yeon (KSLV Systems Devision, Korea Aerospace Research Institute) ;
  • Joh, Miok (KSLV Systems Devision, Korea Aerospace Research Institute)
  • 발행 : 2006.01.31

초록

Development of launch vehicle needs a large-scale and complicated System Engineering discipline interfacing to small-quantity production with special manufacturing processes. In general, the System Engineering discipline of launch vehicle has its relationship with Production, Operations, Product Assurance and Management disciplines and its internal partitions into the functions of System Engineering Integration & Control, Requirements Engineering, Analysis, Design and Configuration and Verification. As a function of Product Assurance, reliability of launch vehicle plays an significant role in risk management, system safety, flight safety and launch certification through design assurance. Moreover, major functions of systems engineering are integrated by means of reliability in the phases of design and verification. Therefore, derailed identification of system engineering interfaces of reliability, and execution of tasks for reliability assurance is required for successful development of launch vehicle. This paper identifies specific pattern and mechanism of the interfaces between reliability and system engineering.

키워드