| 液体推进剂火箭爆炸毒源强度研究 |
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| 引用本文： | 胡世祥,车著明,佘春东.液体推进剂火箭爆炸毒源强度研究[J].宇航学报,2000,21(4):134-139. |
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| 作者姓名： | 胡世祥 车著明 佘春东 |
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| 作者单位： | 1. 中国人民解放军总装备部
2. 四川省西昌市16信箱8号,西昌,615000 |
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| 摘 要： | 在国内外研究液体推进剂爆炸火球生长规律的基础上「１－４，６」，建立了火箭爆炸事故所形成的火球的生长规律、空气卷入量和Ｎ２Ｏ４富余量的数学模型。利用已有的蒸发理论「５」，探讨了火箭发射事故毒源强度及其衰减的计算数学模型。文中所建的数学模型，其试算结果与曾发生过的火箭爆炸事故的火球照片和毒源强度基本匹配。
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| 关 键 词： | 液体推进剂火箭 爆炸事故 火球生成 毒源强度 |
| 修稿时间： | : |
THE EXPLOSIVE TOXICITY SOURCE INTENSITY RESEARCH FOR LIQUID PROPELLANT ROCKET |
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| Hu Shixing,Che Zhuming,She ChunDong.THE EXPLOSIVE TOXICITY SOURCE INTENSITY RESEARCH FOR LIQUID PROPELLANT ROCKET[J].Journal of Astronautics,2000,21(4):134-139. |
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| Authors: | Hu Shixing Che Zhuming She ChunDong |
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| Abstract: | Based on research of the explosive firedball's growing rule for liquid propellant rocket about domestic and abroad,math's models about the explosive fireball's growing rule and about the quantity of the air being involved in and about the surplus of N 2O 4 is established.In the light of evaporate theory of reference 5] ,math's models about the explosive toxicity source intensity and it's decline is explored.The math's model is essential identical with the fireball photograph and the toxicity source intensity of accident that had happened. |
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| Keywords: | Liquid propellant\ Explosion\ Rocket |
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