| 叠氮粘合剂推进剂热分解及燃烧性能研究综述 |
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| 引用本文： | 庞爱民.叠氮粘合剂推进剂热分解及燃烧性能研究综述[J].固体火箭技术,1998,21(4):26-30. |
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| 作者姓名： | 庞爱民 |
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| 作者单位： | 中国航天工业总公司四院四十二所 |
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| 摘 要： | 综述了叠氮类粘合剂ＧＡＰ，ＢＡＭＯ和ＡＭＭＯ的热分解及共推进剂的燃烧性能，认为叠氮类推进剂中－Ｎ３基受热易分解，因而基础燃速高，燃速温度敏感性大；在配方中引入有效的添加剂，可提高该类推进剂的燃速，降低其压强度指数。
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| 关 键 词： | 叠氮化物 推进剂粘合剂 高能推进剂 性能研究 |
Review of Thermal Decomposition and Combustion Properties of Azide Propellants |
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| Pang Aimin.Review of Thermal Decomposition and Combustion Properties of Azide Propellants[J].Journal of Solid Rocket Technology,1998,21(4):26-30. |
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| Authors: | Pang Aimin |
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| Abstract: | The thermal decomposition of azide binders such as GAP, BAMO and AMMO and the combustion properties of azide propellants are reviewed. Because of azide group contained in it , the propellants have higher basic burning rate as well as higher temperature sensitivity. Adding some special catalysts in formulae can increase the burning rate and decrease the pressure exponent of the propellants |
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| Keywords: | Azide Propellant binder High energy propellant Thermal decomposition Burning rate Catalyst |
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