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高能固体推进剂燃速压力指数的分析
引用本文:侯竹林,冯增国.高能固体推进剂燃速压力指数的分析[J].推进技术,1991,12(5):40-44,70.
作者姓名:侯竹林  冯增国
作者单位:北京理工大学 (侯竹林),北京理工大学(冯增国)
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  燃烧速度  压力指数  双基推进剂

ANALYSIS OF THE BURNING-RATE PRESSURE EXPONENT FOR HIGH ENERGY SOLID PROPELLANT
Hou Zhulin and Feng Zengguo.ANALYSIS OF THE BURNING-RATE PRESSURE EXPONENT FOR HIGH ENERGY SOLID PROPELLANT[J].Journal of Propulsion Technology,1991,12(5):40-44,70.
Authors:Hou Zhulin and Feng Zengguo
Institution:Beijing Institute of Technology
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.
Keywords:Propellant pressure exponent  Propellant burning rate  Modified composite double-base propellant  
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