| 摘要: |
| 通过对超高燃速推进剂 (UHBRP)燃速压力曲线的理论分析 ,提出了一种降低UHBRP表观燃速压力指数的技术途径。实验上采取密度梯度的方法制造药柱 ,用大容量密闭爆发器测定了密度梯度药柱的燃速 ,得到了几乎平台型的燃速压力曲线。达到降低UHBRP表观燃速压力指数的目的 ,数据重复性良好 |
| 关键词: 超高燃速推进剂 平台推进剂 推进剂燃烧 压力指数 |
| DOI： |
| 分类号:V512 |
| 基金项目: |
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| Reducing apparent burning rate pressure exponent of ultra high burning rate propellant |
|
Li Xiao Dong, Yang RongJie, Li JianMin, He Jiyu
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Coll. of Chemical Engineering and Material Science, Beijing Inst. of Technology, Beijing, 100081,China
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| Abstract: |
| The characteristic burning rate ( u ) pressure ( p ) curves of ultra high burning rate propellant (UHBRP) were analyzed theoretically. A technological method to reduce the apparent burning rate pressure exponent of UHBRP was used in preparation of UHBRP pellets. A large volume closed bomb was used to measure the burning rates of the UHBRP samples. The u p curves of UHBRP of density gradient show the plateau combustion characteristics. |
| Key words: Superhigh burning rate propellant Mesa burning propellant Propellant combustion Pressure exponent |
