| 含催化剂RDXCMDB推进剂燃烧机理研究 |
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| 引用本文： | 赵凤起,李丽,李上文,阴翠梅,王瑛.含催化剂RDXCMDB推进剂燃烧机理研究[J].固体火箭技术,1999(1). |
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| 作者姓名： | 赵凤起 李丽 李上文 阴翠梅 王瑛 |
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| 作者单位： | 西安近代化学研究所 |
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| 摘 要： | 利用常压ＤＳＣ及ＴＧ／ＤＴＧ，高压ＤＳＣ，单幅照相和燃烧波温度分布测试技术对含ＲＤＸ的复合改性双基推进剂（ＲＤＸＣＭＤＢ）含和不含催化剂时的燃烧机理进行了研究，得到了该种推进剂在热分解和燃烧方面的一些重要结果。
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| 关 键 词： | 黑索今 复合改性双基推进剂 催化 燃烧 |
Research on Combustion Mechanism of RDX CMDB Propellants with or without Catalysts |
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| ZHAO Feng qi,LILi,LI Shang wen,YIN Cui mei,WANG Ying.Research on Combustion Mechanism of RDX CMDB Propellants with or without Catalysts[J].Journal of Solid Rocket Technology,1999(1). |
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| Authors: | ZHAO Feng qi LILi LI Shang wen YIN Cui mei WANG Ying |
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| Abstract: | By using DSC and TG/DTG,high pressure DSC,combustion flame photo analysis and W Re micro thermocouple technology,the combustion mechanism of RDX CMDB propellants with or without composite catalysts was investigaed.Some important results in the respects of the thermal decomposition and combustion were obtained. |
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| Keywords: | Hexogen Modified composite double base propellant Catalysis Combustion |
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