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NEPE推进剂燃烧机理研究
Study on Combustion Mechanism of NEPE Propellant
【摘要】 应用微热电偶测温和燃烧火焰单幅照相技术测得 NEPE推进剂在稳态燃烧条件下的燃烧波温度分布及火焰结构 ,研究了该推进剂中主要组分对燃烧性能的影响 ,同时利用扫描电镜 -能谱仪观测了熄火表面形貌和元素分布规律。经过综合分析 ,提出了 NEPE推进剂的燃烧过程 ,为该类推进剂燃烧物理模型的建立奠定了基础
【Abstract】 The combustion wave temperature profiles and the flame structures of NEPE propellant samples are measured by using W Re micro thermalcouple and flame photo techmique. The influence of major component of propellant (such as HMX,AP,Al)on the combustion properties is researched; Meanuhile the surface appearance and element distribution of extinguished samples are analyzed by JMS 5800 SEM. The combustion process of NEPE propellant is suggested by synthetic analysis.
【关键词】 推进剂;
燃烧机理;
微热电偶;
火焰结构;
【Key words】 Propellant; Combustion mechanism; Micro thermalcouple; Flame structu$;
【Key words】 Propellant; Combustion mechanism; Micro thermalcouple; Flame structu$;
【基金】 火炸药燃烧国防科技重点实验室基金项目
- 【文献出处】 火炸药学报 ,Chinese Journal of Explosives & Propellants , 编辑部邮箱 ,2000年04期
- 【被引频次】26
- 【下载频次】390