ducted rocket propulsion system 冲压火箭发动机
ducted-rocket engine 冲压式火箭发动机
ducted rocket engine 冲压火箭发动机 ; 火箭冲压发动机
ducted rocket motor 火箭冲压发动机
solid ducted rocket 固体火箭冲压发动机燃烧室
solid ducted rocket sdr 固体火箭冲压发动机
solid ducted rocket motor 固体火箭冲压发动机
solid ducted rocket engine 固体火箭冲压发动机
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 effects of various parameters on boron particle ignition of ducted rocket secondary chamber were studied with the model developed by the King.
硼颗粒在通过固体火箭冲压发动机的燃气发生器喷管进入补燃室的过程中，颗粒通常都会受到高速气流的作用。
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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