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固体火箭发动机可靠性增长试验规划初步研究 被引量:1

Primary Research on Reliability Growth Test Program for Solid Rocket Motor
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摘要 研究了固体火箭发动机产品总数一定情况下可靠性增长试验量的确定问题.提出了模型假设,以剩余产品成功数期望值最大作为目标函数,建立数学模型;然后,在初始故障数服从泊松分布时,推导了确定可靠性增长试验量的极大-极小准则,给出了产品研制后期故障数的替代分布.最后给出了一个应用实例,结果表明该准则有点保守,但较为稳健. How to decide the number of reliability growth tests for solid rocket motor is researched when the total of products is fixed. The model hypothesises are proposed, and the initial mathematics model is established. Thus, the max-min rule for reliability growth test is deduced when the initial potential bugs or faults is subject to Poisson distribution. An example is shown to illustrate this method. It is indicated that the rule is somewhat conservative, but quite robust.
机构地区 中国人民解放军
出处 《战术导弹技术》 北大核心 2007年第6期1-3,共3页 Tactical Missile Technology
基金 国防预研基金项目
关键词 固体火箭发动机 成败型 可靠性增长试验 泊松分布 极大-极小停止准则 solid propellant rocket engine success-failure reliability growth test Poisson distribution max-min stopping rule
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参考文献4

  • 1Seglie E.How Much Testing Is Enough?[].the"Workshop on Statistical Issues in De-fense Analysis and Testing.1992
  • 2Mu-Yeh Huang.Design of Developmental Test Programsfor One-shot Systems with Two State Reliability[]..1995
  • 3Mu-Yeh Huang,Douglas McBeth,Stephen B Vardeman.Development Test Results[].IEEE Transactions on Re-liability.1995
  • 4Gaver D P,Jacobs P A.Testing or Fault-finding for Reli-ability Growth:A Missile Destructive-test Example[].Quality and Reliability.1997

同被引文献4

  • 1SEGLIE E. How much testing is enough[R]//Paper Presented at the "Workshop on Statistical Issues in Defense Analysis and Testing" Sponsored by the National Research Council. Washington, D.C., 1992.
  • 2MU-YEH HUANG, Douglas MeBeth, Stephen B.Vardeman. Development test results[J]. IEEE Transactions on Reliability, 1995,3(45): 189-198.
  • 3MU-YEH HUANG. Design of programs for one-shot system reliability[D]. Lowa State Universi developmental test s with two statety, 1995.
  • 4GAVER D P, JACOBS P A. Probability models for sequential-stage system reliability growth via failure mode removal[J]. International Journal of Reliability, Quality and Safety Engineering, 2003,10(1): 15-40.

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