Volume 26 Issue 4
Apr.  2011
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LI Jin, ZHAO Yu, LI Wen-zhao, YANG Jun. Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors[J]. Journal of Aerospace Power, 2011, 26(4): 931-934.
Citation: LI Jin, ZHAO Yu, LI Wen-zhao, YANG Jun. Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors[J]. Journal of Aerospace Power, 2011, 26(4): 931-934.

Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors

  • Received Date: 2010-03-18
  • Rev Recd Date: 2010-11-16
  • Publish Date: 2011-04-28
  • The problem of liquid-propellant rocket engine's reliability compliance test plans at present is that ignoring the processes of firing and shutdown or the test taking too long.To solve this problem,considering typical compliance test plans of binomial distribution and Weibull distribution,using the weighting factors,the method of reliability compliance test plan developing was provided.The duration of firing was verified in this reliability compliance test plans developing method,at the same time the processes of firing and shutdowns were also considered.This reliability compliance test plan utilized development information and saved the test time and cost.

     

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  • [1]
    Committee of G-11 Reliability Maint Support and Probabilistic Methods.ARP4900 Liquid rocket engine reliability certification[S].USA:SAE International,1996.
    [2]
    冯静,刘琦,周经纶,等.基于最优置信限法的液体火箭发动机可靠性鉴定验收方案[J].质量与可靠性,2003(1):29-32. FENG Jing,LIU Qi,ZHOU Jinglun,et al.The reliability qualification test plan for liquid rocket engine based on optimal confidence limit method[J].Quality and Reliability,2003(1):29-32.(in Chinese)
    [3]
    Lloyd D K,Lipow M.Reliability:management,methods, and mathematics[M] .New Jersey:Prentice-Hall Inc., 1962.
    [4]
    Pugh R L.Space transportation main engine reliability demonstration technique //Proceedings Annual Reliability and Maintainability Symposium.Atlanta:IEEE,1993:173-180.
    [5]
    Committee of DS/1 Dependability and terotechnology.BS EN 61649:2008 Weibull analysis[S].UK:BSI,2009.
    [6]
    贺国芳.可靠性数据的收集与分析[M].北京:国防工业出版社,1995.
    [7]
    王婷婷,师义民,刘英.某型号液体火箭发动机可靠性分析[J].航天控制,2009,27(6):79-82. WANG Tingting,SHI Yimin,LIU Ying.Reliability analysis for a kind of liquid rocket[J].Aerospace Control,2009,27(6):79-82.(in Chinese)
    [8]
    宁江凡,鄢小清,张士峰.液体火箭发动机无失效条件下的可靠性分析方法[J].国防科技大学学报,2006,28(5):22-25. NING Jiangfan,YAN Xiaoqing,ZHANG Shifeng.Study on reliability anlysis method for liquid rocket engine in the case of zero-failure data[J].Journal of National University of Defense Technology,2006,28(5):22-25.(in Chinese)
    [9]
    刘琦,冯静,周经纶.基于Gompertz模型的液体火箭发动机可靠性增长分析[J].航空动力学报,2004,19(3):419-423. LIU Qi,FENG Jing,ZHOU Jinglun.The reliability growth analysis for liquid rocket engine according to the Gompertz model[J].Journal of Aerospace Power,2004,19(3):419-423.(in Chinese)
    [10]
    姜祥周,师义民,沈政.无失效数据下液体火箭发动机可靠性多层Bayes估计[J].航空控制,2008,26(3):88-91. JIANG Xianzhou,SHI Yimin,SHEN Zheng.The hierarchical Bayes reliability estimation for liquid rocket engine with zero-failure data[J].Aerospace Control,2008,26(3):88-91.(in Chinese)
    [11]
    李宝盛,郝京辉.液体火箭发动机寿命可靠性的贝叶斯下限[J].导弹与航天运载技术,2009(4):8-10. LI Baosheng,HAO Jinghui.Bayesian lower limit of life-time reliability for liquid propellant rocket engine[J].Missile and Space Vehicle,2009(4):8-10.(in Chinese)
    [12]
    Murphy T,Voss N.Liquid rocket engine acceptance testing:improved system reliability without hotfire //Proccedings of 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference.Lake Buena Vista:AIAA,1996:1-6.
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