| Ap／RDX推进剂燃速调节实验研究 |
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| 引用本文： | 刘德辉,黄少波.Ap／RDX推进剂燃速调节实验研究[J].固体火箭技术,1994,17(2):40-45. |
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| 作者姓名： | 刘德辉 黄少波 |
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| 作者单位： | 国防科技大学，国防科技大学，国防科技大学 湖南长沙 410073，湖南长沙 410073，湖南长沙 410073 |
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| 摘 要： | 利用正交试验法研究了CuO、Cr_2O_3和Fe_2O_3三种催化剂对Ap/RDX推进剂燃烧性能的影响,得到了提高燃速的最佳催化剂组合,提出了催化剂对Ap/RDX推进剂的催化机理,该机理可较好地解释许多实验结果。
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| 关 键 词： | 火箭推进剂 硝胺催化剂 推进剂燃速 |
Experimental Investigation on Burning Rate Modification of Ap/RDX Propellants |
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| Liu Dehui Huang Shaobo Zhang Lixin.Experimental Investigation on Burning Rate Modification of Ap/RDX Propellants[J].Journal of Solid Rocket Technology,1994,17(2):40-45. |
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| Authors: | Liu Dehui Huang Shaobo Zhang Lixin |
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| Abstract: | The effects of three catalysts (CuO, Cr2O3and Fe2O3) on combustion performance of Ap / RDX propellants have been in vestigated by means of the orthogonal-test method, and the optimum formation of catalysts to increase the burning rate is obtained. A catalytical mechanism of the catalyst for Ap / RDX propellants, which can be used for explaining many experimental results satisfactorily, has been presented based on the analyses and discussions. |
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| Keywords: | Solid rocket propellant Nitramine propellant Propellant burning rate Combustion catalyst |
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