| 铝粉粒径及形状对HTPB推进剂力学性能的影响 |
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| 引用本文： | 丁世俊 鲁国林. 铝粉粒径及形状对HTPB推进剂力学性能的影响[J]. 固体火箭技术, 1994, 17(4): 43-49 |
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| 作者姓名： | 丁世俊 鲁国林 |
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| 作者单位： | 四院四十二所，四院四十二所，四院四十二所 湖北襄樊 441003，湖北襄樊 441003，湖北襄樊 441003 |
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| 摘 要： | 铝粉球形化显著地改善了推进剂的力学性能;然而推进剂的燃速明显地降低。可通过调节球形Ap D_(43)粒径法提高燃速。用1~#球形铝粉代替1~#或3~＃非球形铝粉时,推进剂的常温伸长率分别提高4.0％～8.0％或8.0％～14.0％。
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| 关 键 词： | 含铝 推进剂 端羟基聚丁二烯 燃速 力学性能 |
The Effects of Aluminum Powder Diameter and Form on Mechanical Properties of the HTPB Propellant |
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| Ding Shijun Lu Guolin Liu Yuehua. The Effects of Aluminum Powder Diameter and Form on Mechanical Properties of the HTPB Propellant[J]. Journal of Solid Rocket Technology, 1994, 17(4): 43-49 |
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| Authors: | Ding Shijun Lu Guolin Liu Yuehua |
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| Abstract: | The spherical aluminum powder improves mechanical properties of the propellant. However, the buring rate of the propellant decrease. By adjusting D43 of the spherical Ap, the buring rate of the propellant is increased. The spherical aluminum powder 1 instead of non-spherical aluminum powder 1 or 3 can improve the extensibility of the propellant at normal temperature by about 4.0%-14.0% or 8.0-14.0%. |
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| Keywords: | Aluminized propellant Hydroxy terminated polybutadiene propellant Burning rate Extensibility |
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