Configuration Management System for Rotorcraft Multi-Component Developement

회전익기 다품종부품 개발을 위한 형상관리 체계

  • 김현기 (한국항공우주연구원 항공계통팀) ;
  • 김학범 (한국항공우주연구원 항공계통팀) ;
  • 김성찬 (한국항공우주연구원 항공계통팀)
  • Received : 2012.08.20
  • Accepted : 2012.09.19
  • Published : 2012.09.30


Medium size rotorcraft consist of approximately 5,000 key components. The components must satisfy the target weight and performance requirement through optimization. Therefore a rotorcraft component has approximately 100 times higher unit cost for mass production than the equivalent of an automobile's, along with huge development cost. Configuration management consists of four main parts : configuration identification, configuration control, configuration audit, and data management. In development programme, configuration management is one of the methods to save development cost, and setting a well-structured configuration management system according to the Military Standard is an important factor in success of the programme. The paper proposes a configuration management system suitable for development of various multi-use components development and presents that the configuration management was performed successfully during dual-use component development programme using the established system.


Supported by : 지식경제부


  1. MIL-STD-973, "Configuration Management", Military Standard, 1992
  2. MIL-HDBK-61, "Configuration Management Guidence", Military Handbook, 20011963, pp.334-338.