| 舰载导弹固体发动机发射跌落危险性分析 |
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| 引用本文： | 杨明,黄卫东,李高春,李金飞.舰载导弹固体发动机发射跌落危险性分析[J].海军航空工程学院学报,2018,33(4):367-370, 400. |
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| 作者姓名： | 杨明 黄卫东 李高春 李金飞 |
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| 作者单位： | 海军航空大学;航天工程大学 |
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| 摘 要： | 为了研究舰载导弹固体发动机冷弹射点火失败后跌落的安全性问题,采用推进剂的点火增长模型,利用ANSYS/LS-DYNA软件计算发动机垂直跌落过程。结果表明,发动机的尾部、壳体和装药的应力均很大,有产生破坏的风险,推进剂的温升较小,不会发生点火反应,但其应变较大,存在产生大变形破坏的可能性。
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| 关 键 词： | 固体发动机 推进剂 跌落 安全性 点火增长模型 |
Launching Drop Risk Analysis of Shipborne Missile Solid Motor |
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| YANG Ming,HUANG Weidong,LI Gaochun and LI Jinfei.Launching Drop Risk Analysis of Shipborne Missile Solid Motor[J].Journal of Naval Aeronautical Engineering Institute,2018,33(4):367-370, 400. |
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| Authors: | YANG Ming HUANG Weidong LI Gaochun and LI Jinfei |
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| Institution: | Naval Aviation University, Yantai Shangdong 264001, China,Aerospace Engineering University, Beijing 100000, China,Naval Aviation University, Yantai Shangdong 264001, China and Naval Aviation University, Yantai Shangdong 264001, China |
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| Abstract: | In order to study the safety of shipborne missile solid rocket motor (SSM) dropping after failure of cold ejectionignition, the ignition growth model of propellant was used to calculate the vertical dropping process of SSM using ANSYS/LS-DYNA software. The results show that the stresses in the tail, shell and charge of the engine are very large, and there isa risk of damage. The temperature rise of the propellant is small, and there is no ignition reaction, but the strain is large,and there is a possibility of large deformation damage. |
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| Keywords: | solid rocket motor propellant drop safety ignition growth model |
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