| 摘要: |
| 本文根据双基系列推进剂的发展与演变,在实验的基础上分析了影响CMDB推进剂燃速压力指数的各种因素并推论了降低高能固体推进剂压力指数的具体措施,这些讨论对于新一代硝酸酯增塑的聚醚聚氨酯推进剂燃烧性能的研究具有指导意义. |
| 关键词: 推进剂燃速 推进剂压力指数 复合改性双基推进剂 |
| DOI： |
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| ANALYSIS OF THE BURNING-RATE PRESSURE EXPONENT FOR HIGH ENERGY SOLID PROPELLANT |
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Hou Zhulin, Feng Zengguo
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Beijing Institute of Technology
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| Abstract: |
| Based on the evolution of double-base(DB)propellants, the effect of various factors on burning-rate pressure exponent and the detailed methods for decreasing the pressure exponent for high energy solid propellant are discussed in terms of the experimental data. These discussions are useful for studying the characteristics of a new generation of high energy solid pro-pellant-polyether polyurethane propellant plasticized by nitrate esters. |
| Key words: Propellant pressure exponent Propellant burning rate Modified composite double-base propellant |
