Method of Estimating Environment Conversion Factor Analyzing Environment Factors of MIL-HDBK-217F

MIL-HDBK-217F의 환경인자 분석을 통한 환경변환계수 추정

  • Jeong, Da-Un (Maintenance Technology Research Center, Consolidated Maintenance Depot, ROK Army) ;
  • Yun, Hui-Sung (Maintenance Technology Research Center, Consolidated Maintenance Depot, ROK Army) ;
  • Lee, Eun-Hak (Maintenance Technology Research Center, Consolidated Maintenance Depot, ROK Army) ;
  • Kwon, Dong-Soo (Maintenance Technology Research Center, Consolidated Maintenance Depot, ROK Army) ;
  • Lee, Seung-Hun (Maintenance Technology Research Center, Consolidated Maintenance Depot, ROK Army)
  • 정다운 (육군 종합정비창 정비기술연구소) ;
  • 윤희성 (육군 종합정비창 정비기술연구소) ;
  • 이은학 (육군 종합정비창 정비기술연구소) ;
  • 권동수 (육군 종합정비창 정비기술연구소) ;
  • 이승헌 (육군 종합정비창 정비기술연구소)
  • Received : 2011.03.23
  • Accepted : 2011.06.03
  • Published : 2011.06.25

Abstract

Environment Conversion Factors, which are stipulated in System Reliability Toolkit, have a lot of advantages once applied in a reliability data handbook such as NPRD-95, during the process of reliability prediction. However, the factors have a restriction in their applications because they don't deal with a few environments, e.g., Missile Launch (ML). In this study, environment factors of various components from MIL-HDBK-217F were analyzed to address this problem. Statistical computations showed that converting from Airborne Rotary Wing (ARW) to Missile Launch (ML) was the most coherent by comparing coefficient of determination. In addition, conversion factors from System Reliability Toolkit and those from the statistical calculations were evaluated in terms of their similarities.

Keywords

References

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