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铝镁贫氧推进剂低压燃烧性能表征方法研究
引用本文:张炜,朱慧.铝镁贫氧推进剂低压燃烧性能表征方法研究[J].含能材料,2002,10(3):125-127.
作者姓名:张炜  朱慧
作者单位:国防科技大学航天与材料工程学院,湖南,长沙,410073
基金项目:国防预研基金资助项目(99J12.6.8.KG0128)
摘    要:系统研究了铝镁贫氧推进剂低压燃烧性的表征方法。研究发现,低压下采用表压和绝压强所得到的燃速压强指数不同,用Summerfield燃速公式回归燃速与压强的关系比Vieille燃速公式更好一些。

关 键 词:铝镁贫氧推进剂  低压  燃烧性能  表征方法  非壅塞固体火箭冲压发动机
文章编号:1006-9941(2002)03-0125-03
收稿时间:2002/2/20 0:00:00
修稿时间:2002年2月20日

Characterization Methods of Combustion Properties of Aluminum-magnesium Fuel-rich Propellant at Low Pressure
ZHANG Wei and ZHU Hui.Characterization Methods of Combustion Properties of Aluminum-magnesium Fuel-rich Propellant at Low Pressure[J].Chinese Journal of Energetic Materials,2002,10(3):125-127.
Authors:ZHANG Wei and ZHU Hui
Affiliation:Inst. of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China;Inst. of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:The characterization of the combustion properties of the aluminum-magnesium fuel-rich propellant for unchoked ducted rocket was studied. The pressure exponents calculated by the burning rates at different pressure from the pressure gauge and from the absolute pressure are different. The author suggested using the exponents calculated from the absolute pressure. The experimental results show that the correlation between the burning rate and the pressure is better suited by the Summerfield formula than the Vieille Law.
Keywords:aluminum-magnesium fuel-rich propellant  low pressure  characterization of combustion property
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