| 固体火箭发动机不点火自毁爆炸危险性研究 |
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| 引用本文： | 殷雅侠,刘平,谷乃古.固体火箭发动机不点火自毁爆炸危险性研究[J].固体火箭技术,2004,27(2):111-113. |
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| 作者姓名： | 殷雅侠 刘平 谷乃古 |
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| 作者单位： | 中国航天科技集团公司四院,西安,710025 |
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| 摘 要： | 根据中能固体火箭发动机的自毁爆炸特点及发动机自毁模拟试验的结果。结合过去固体火箭发动机的研制经验。提出了中能固体发动机不点火自毁爆炸危险性的计算方法。并对三级火箭固体火箭发动机不点火自毁时的爆炸TNT当量，碎片飞散距离和冲击波超压安全距离进行了计算和分析，为导弹自毁爆炸危险性分析提供了参考。
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| 关 键 词： | 固体火箭发动机 不点火自毁 爆炸危险性 线形爆炸器 联合自毁 柱形爆炸器 |
| 文章编号： | 1006-2793(2004)02-0111-03 |
| 修稿时间： | 2003年4月14日 |
Study on the non-ignition self-destruction explosion hazard of SRM |
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| YIN Ya-xia,LIU Ping,GU Nai-guThe Fourth Academy of CASC,Xi'an ,China.Study on the non-ignition self-destruction explosion hazard of SRM[J].Journal of Solid Rocket Technology,2004,27(2):111-113. |
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| Authors: | YIN Ya-xia LIU Ping GU Nai-guThe Fourth Academy of CASC Xi'an China |
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| Institution: | YIN Ya-xia,LIU Ping,GU Nai-guThe Fourth Academy of CASC,Xi'an 710025,China |
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| Abstract: | Based on the self-destruction explosion characteristics and self-de-struction simulation test results of medium energy solid propellant rocket motor ,with reference of the development experience of SRMs, the non-ignition self-destruction explosion hazard calculative method of medium energy SRM was put forward .This method was used for calculation and analysis of the explosion TNT equivalent value, the fragment flying distance and the safe distance of blast wave overpressure when the three stages SRMs were destructed because of the ignition failuare. The results can give a reference to the self-destruction explosion hazard analysis of a missile. |
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| Keywords: | solid rocket motor non-ignition self-destruction explosion hazard |
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