| 国外战术导弹固体火箭发动机低易损性技术分析 |
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| 引用本文： | 戴耀松.国外战术导弹固体火箭发动机低易损性技术分析[J].推进技术,1998,19(1):99-102. |
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| 作者姓名： | 戴耀松 |
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| 作者单位： | 航天工业总公司31所,北京,100074 |
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| 摘 要： | 评述了１９８５年以来国外低易损性和钝感技术的研究进展；分析对比了低易损性实验技术和小规模实验室试验方法；讨论了最近使用危险性评估协议的活动。此外，还介绍了低易损性固体发动机的设计技术，并对我国发展战术导弹固体发动机低易损性研究和设计的问题提出了建议。
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| 关 键 词： | 固体火箭发动机 易损性 推进剂感度 导弹 |
THE LOW VULNERABILITY OF SOLID ROCKET ENGINE FOR TACTICAL MISSILE |
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| Dai Yaosong.THE LOW VULNERABILITY OF SOLID ROCKET ENGINE FOR TACTICAL MISSILE[J].Journal of Propulsion Technology,1998,19(1):99-102. |
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| Authors: | Dai Yaosong |
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| Affiliation: | The 31st Research Institute,Beijing,100074 |
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| Abstract: | The low vulnerability of solid rocket engine is an important performance in relations to munitions survivability Development of low vulnerabilty and insensitive munitions since 1985 is described,which includes analysis and comparison of methods of subscale laboratory tests The hazard assessment protocols,hot fragment ignition threat/response and low vulnerability design are discussed Finally,policy and way of further research and deveopment of low vulnerability solid rocket engine are proposed |
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| Keywords: | Solid propellant rocket engine Vulnerability Propellant sensitivity Safety test Missle accident |
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