| 固体火箭发动机结构可靠性评估方法的探讨 |
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| 引用本文： | 施灵,赵福祥.固体火箭发动机结构可靠性评估方法的探讨[J].上海航天,1999,16(4):37-41. |
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| 作者姓名： | 施灵 赵福祥 |
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| 作者单位： | 上海航天技术研究院８１０所(施灵)，空军驻上海航天技术研究院８１０所军事代表室(赵福祥) |
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| 摘 要： | 对战术导弹固体火箭发动机的结构可靠性评估方法及其应用作了述评，并以某空空导弹发动机为例进行了计算、比较。与其他方法相比，有验前信息的贝叶斯法能较好地反映发动机的实际结构可靠性水平，是一种较为合理、有效的评估方法，并提出了基于应力－强度干涉仪模型的变量分析法将是发动机结构可靠性评估的一个发展方向
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| 关 键 词： | 战术导弹 固体火箭发动机 结构可靠性 评估方法 |
INVESTIGATION OF ASSESSMENT FOR STRUCTURAL RELIABILITY OF TACTIC MISSILE SOLID ROCKET MOTOR |
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| SHI Ling ,ZHAO Fu xiang.INVESTIGATION OF ASSESSMENT FOR STRUCTURAL RELIABILITY OF TACTIC MISSILE SOLID ROCKET MOTOR[J].Aerospace Shanghai,1999,16(4):37-41. |
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| Authors: | SHI Ling ZHAO Fu xiang |
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| Institution: | SHI Ling 1,ZHAO Fu xiang 2 |
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| Abstract: | In this paper,some assessments for structural reliability of tactic missile solid rocket motors and their applications are reviewed. Some calculations and comparisons are made based on the firing test results of some air air missile motor. The more rational, effective assessment is in the engineering development of solid rocket motor and a developing tendency in the future are presented. |
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| Keywords: | Tactic missile Solid rocket motor Structural reliability Assessment |
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