| 固体火箭发动机可靠性评定技术 |
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| 引用本文： | 刘朋,张平.固体火箭发动机可靠性评定技术[J].固体火箭技术,2002,25(1):1-4. |
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| 作者姓名： | 刘朋 张平 |
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| 作者单位： | 北京理工大学机电工程学院,北京,100081 |
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| 摘 要： | 分析了固体火箭发动机可靠性评定的主要方法，并简要分析了固体火箭发动机可靠性评定中的某些关键技术及其发展动向，如失效模式和故障判据的选用，复杂承载条件下的应用计算，可靠性模型的建立以及先进算法在可靠性评定中的应用等。
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| 关 键 词： | 火箭发动机 可靠性评价 失效模式 故障 诊断 |
| 文章编号： | 1006-2793(2002)01-0001-04 |
| 修稿时间： | 2001年9月21日 |
The technologies of reliability assessment of solid rocket motors |
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| LIU Peng,ZHANG Ping//School of Mechano Electronics Engineering,Beijing Institute of Technology.The technologies of reliability assessment of solid rocket motors[J].Journal of Solid Rocket Technology,2002,25(1):1-4. |
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| Authors: | LIU Peng ZHANG Ping//School of Mechano Electronics Engineering Beijing Institute of Technology |
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| Institution: | LIU Peng,ZHANG Ping//School of Mechano Electronics Engineering,Beijing Institute of Technology. Beijing 10081,China. |
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| Abstract: | This paper introduces the key technologies on reliability assessment of solid rocket motors including reliability assessment methods, selection of failure modes and failure criterion, calculation of stress, establishment of reliability assessment modes, application of computer and so on. The paper also analyzes the trends of these technology developments. |
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| Keywords: | solid propellant rocket engine reliability assessment failure mode failure diagnosis |
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