- Volume 20 Issue 3
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Configuration Management System for Rotorcraft Multi-Component Developement
회전익기 다품종부품 개발을 위한 형상관리 체계
- 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
- MIL-STD-973, "Configuration Management", Military Standard, 1992
- MIL-HDBK-61, "Configuration Management Guidence", Military Handbook, 20011963, pp.334-338.