| 硝基立方烷及其氮杂衍生物的能量特性计算研究 |
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| 引用本文： | 郑剑.硝基立方烷及其氮杂衍生物的能量特性计算研究[J].固体火箭技术,1995,18(1):45-53. |
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| 作者姓名： | 郑剑 |
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| 作者单位： | 湖北襄樊四院四十二所 |
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| 摘 要： | 硝基立方烷及其氮杂衍生物是高能量密度材料的重要目标化合物类型之一。据此详细计算分析了硝基立方烷（从二硝基到八硝基立方烷）和四硝基四氮的杂立方烷分别在产单元推进剂，ＨＴＰＢ／Ａｌ，ＰＥＧ／ＮＧ／Ａｌ，ＧＡＰ／ＮＧ／Ａｌ体系中的能量特性。结果表明，硝基取代数大于４的立方烷和四硝基四氮杂立方烷的能量特性明显优于ＨＭＸ。
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| 关 键 词： | 高能材料 固体推进剂 硝基立方烷 氮杂衍生物 |
The Computational Investigation of Energetic Performances of Nitrocubanesand Nitroazacubanes |
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| Zheng Jian.The Computational Investigation of Energetic Performances of Nitrocubanesand Nitroazacubanes[J].Journal of Solid Rocket Technology,1995,18(1):45-53. |
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| Authors: | Zheng Jian |
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| Abstract: | Nitrocubanes and nirtoazacubanes are the important target compounds in the field of high energy density materials (HEDM).The energetic performances of the nitrocubanes (from dinitrocubane to octanitrocubane) and tetranitrotetraazacubane used in monopropellant,HTPB/Al,PEG/NG/Al and OAP/NG/Al formulations are calculated and discussed in details.The results show that the nitrocubanes with over four nitro-groups and the tetranitrotetraazacubane are obviously superior to HMX in the energetic performances. |
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| Keywords: | Terms Performance prediction High erergy material Solid propellant |
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