The combustion mechanism of boron-based fuel-rich propellant was studied.
含硼富燃推进剂燃烧机理研究。
Thus, improving the condensed-phase reaction can increase of the burning rate for fuel-rich propellant with boron in low pressure condition.
分析表明促进凝相反应有利于含硼富燃料推进剂低压燃速的提高。
The combustion wave temperature profiles and flame structures of fuel-rich propellant containing boron are measured by using W-Re micro-thermal couple and flame photo technique.
通过微热电偶测温和火焰单幅照相技术测试了含硼富燃料推进剂燃烧波温度分布及燃烧火焰结构；
The burning rate of the fuel-rich propellants is the parameter which is important for Ducted Rocket design and performance analysis and is main inspection criterions of propellant prescriptions.
贫氧推进剂燃速是固体火箭冲压发动机设计和性能分析的重要参数，也是对推进剂配方进行检验验收的主要指标。
The characterization of the combustion properties of the aluminum? Magnesium fuel? Rich propellant for unchoked ducted rocket was studied.
系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
The combustion characteristics of silver wire embeded fuel rich propellant grain are investigated.
系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
The characteristics of the boron based fuel rich propellant and its modification techniques are reviewed.
综述了国内外对含硼贫氧推进剂燃烧特性及其改进技术的研究成果。
The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated.
研究了过渡金属氧化物（TMO ）及其复配物对非壅塞固体火箭冲压发动机铝镁贫氧推进剂燃烧特性的影响。研究发现，氧化铁对提高铝镁贫氧推进剂燃速的作用显著。
The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated.
研究了过渡金属氧化物（TMO ）及其复配物对非壅塞固体火箭冲压发动机铝镁贫氧推进剂燃烧特性的影响。研究发现，氧化铁对提高铝镁贫氧推进剂燃速的作用显著。
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