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含镁铝富燃料推进剂低压燃速规律研究
引用本文:庞维强,胥会祥,王国强,樊学忠.含镁铝富燃料推进剂低压燃速规律研究[J].航空计测技术,2008,28(6).
作者姓名:庞维强  胥会祥  王国强  樊学忠
作者单位:西安近代化学研究所,陕西西安710065
基金项目:"十一五"国防科技工业技术基础科研计量项目资助  
摘    要:以成熟的含镁铝富燃料推进剂配方为基础选择制备推进剂的候选物,制备出均匀性和稳定性良好的含镁铝富燃料固体推进剂,并对影响该推进剂的燃速不确定度的因素进行了初步分析.结果表明,所制备的含镁铝富燃料推进剂燃速具有较好的均匀性和稳定性,其扩展不确定度小于2.0(k=2).

关 键 词:镁铝富燃料推进剂  燃速特性  误差分析  不确定度分析

Study of Burning Rate in Low Pressure Mg/Al Fuel-rich Propellant
PANG Wei-qiang,XU Hui-xiang,WANG Guo-qiang,FAN Xue-zhong.Study of Burning Rate in Low Pressure Mg/Al Fuel-rich Propellant[J].Aviation Metrology & Measurement Technology,2008,28(6).
Authors:PANG Wei-qiang  XU Hui-xiang  WANG Guo-qiang  FAN Xue-zhong
Institution:PANG Wei-qiang,XU Hui-xiang,WANG Guo-qiang,FAN Xue-zhong(Xi\'an Modern Chemistry Research Institute,Xi\'an 710065,China)
Abstract:Based on the mature formulation of magnalium fuel-rich propellant,the burning rate of the magnalium fuel-rich propellant with good uniformity and stability has prepared.The effects of various factors for burning rate uncertainty on magnalium fuel-rich propellant are analyzed.The results show that the burning rate of magnalium fuel-rich propellant which we prepared has good uniformity and stability,its extended uncertainty is less than 2.0.
Keywords:magnalium fuel-rich propellant  burning rate property  error analysis  uncertainty analysis  
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