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NEPE高能推进剂力学性能模拟计算
引用本文:贵大勇,刘剑洪,田德余,庞爱民,张小平.NEPE高能推进剂力学性能模拟计算[J].推进技术,2010,31(4):444-447,451.
作者姓名:贵大勇  刘剑洪  田德余  庞爱民  张小平
作者单位:1. 深圳大学,化学与化工学院,广东,深圳,518060
2. 湖北航天化学技术研究所,湖北,襄樊,441003
摘    要:将颗粒填充聚合物三相结构(颗粒相-中间相-基体相)和粘弹模型相结合,提出了NEPE高能固体推进剂三相结构粘弹模型,建立了NEPE高能推进剂力学性能与其配方组成、固体填料粒径及级配、弹性母体(基体)的拉伸强度和模量、界面层模量等参数的数学关系,进行了编程计算,其拉伸强度和伸长率90%的计算值和测试结果相对误差小于20%。

关 键 词:NEPE推进剂  力学性能  模拟

Modeling of mechanical properties of NEPE high energetic propellants
GUI Da-yong,LIU Jian-hong,TIAN De-yu,PANG Ai-min and ZHANG Xiao-ping.Modeling of mechanical properties of NEPE high energetic propellants[J].Journal of Propulsion Technology,2010,31(4):444-447,451.
Authors:GUI Da-yong  LIU Jian-hong  TIAN De-yu  PANG Ai-min and ZHANG Xiao-ping
Institution:1.School of Chemistry and Chemical Engineering,Normal Coll.Shenzhen Univ.,Shenzhen 518060,China;2.Hubei Inst.of Aerospace Chemotechnology,Xiangfan 441003,China)
Abstract:A three-phase viscoelastic constitutive model is proposed and verified for prediction of the mechanical properties of NEPE high energetic propellants.The relationships between mechanical properties of NEPE propellants and the formulation,particle size,gradation,modulus and tensile strength of matrix,etc.are constructed mathematically.The results show that the predictions of this model is in good agreement with experimental measurements for both tensile strength and elongation of NEPE high energetic propellants.
Keywords:NEPE propellants  Mechanical property  Modeling
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