| 宽使用温度范围的丁羟高燃速推进剂配方研究 |
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| 引用本文： | 鲁国林,尹瑞康,刘爚. 宽使用温度范围的丁羟高燃速推进剂配方研究[J]. 推进技术, 2001, 22(2): 162-164 |
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| 作者姓名： | 鲁国林 尹瑞康 刘爚 |
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| 作者单位： | 湖北红星化学研究所, |
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| 摘 要： | 研究了细AP含量、增塑剂癸二酸二异辛酯（DOS）含量和键合剂LW1等因素对HTPB／IPDI高燃烧推进剂－55℃低温力学性能的影响，获得了一个使用范围广（－55℃－＋70℃）、综合性能优良的丁羟高燃速推进剂配方。该推进剂除具有能量高、燃速高等特点外，还有优良的力学性能。70℃最大抗拉强度（σm）蒺、MPa,25℃,70℃最大伸长率（εm）大于45％，－55℃时的伸长率大于30％。
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| 关 键 词： | 端羟基聚丁二烯推进剂 高燃速推进剂 高温推进剂 低温力学性能 |
| 文章编号： | 1001-4055（2001）02-0162-03 |
| 修稿时间： | 2000-03-16 |
High burning rate propellant formulation used in broad temperature range |
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| LU Guo-lin,YIN Rui-kang and Liu Yue. High burning rate propellant formulation used in broad temperature range[J]. Journal of Propulsion Technology, 2001, 22(2): 162-164 |
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| Authors: | LU Guo-lin YIN Rui-kang Liu Yue |
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| Affiliation: | Hubei Red-Star Chemical Inst., Xiangfan 441003,China;Hubei Red-Star Chemical Inst., Xiangfan 441003,China;Hubei Red-Star Chemical Inst., Xiangfan 441003,China |
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| Abstract: | The effects of the contents of fine ammonium perchlorate(AP) and plasticizer di-2-ethylhexyl sebacate(DOS) and bonding agent LW1 on mechanical properties of high burning rate HTPB/IPDI propellant at -55 ℃ were studied.A high burning rate HTPB propellant formulation with better comprehensive properties and used in the -55 ℃～+70 ℃ broad temperature range was gained. Propellant formulation has better mechanical properties except for properties of high burning rate and energy. Maximum tensile strength（σm） of propellant at 70 ℃ is higher than 0.5 MPa. Maximum elongation（εm） at 70 ℃ and 25 ℃ are superior to 45%. Maximum elongation（εm） at -55 ℃ is higher than 30%. |
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| Keywords: | Hydroxy terminated polybutadience propellant High burning rate propellant High temperature propellant Performance of low temperature mechanics |
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