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- Influence of afterburning chamber length on secondary combustion for solid ducted rocket motor 补燃室长度对固冲发动机二次燃烧的影响
- Theoretical analysis on effect of direct heating on ground simulation performance for solid ducted rocket motor 直接加热对固冲发动机地面模拟性能影响的理论分析
- Investigation into the Feasibility of Boron Powder Burning in the Second Combustor of Ducted Rocket Motor 硼粉在冲压发动机补燃室中可燃性研究
- Ducted Rocket Motor 冲压火箭复合式发动机
- solid ducted rocket motor 固体火箭冲压发动机
- Effects of the angles of binary air-inlets on after-burning of ducted rocket motors 二元进气道夹角对冲压发动机二次燃烧的影响
- At first, the thermodynamic calculation of Solid Ducted Rocket is researche. 在此基础上，首先对固体冲压发动机热力计算展开了研究分析。
- Rocket motor cases and the specially designed production equipment therefor. 四、火箭发动机的壳体及为其专门设计的生产设备。
- Stowe R A, Champlain A De, Mayer A E H J. Modeling combustor performance of a ducted rocket[R]. AIAA paper 2000-3728. 张炜;方丁酉;夏智勋;等.;非壅塞固体火箭冲压发动机工作特性研究[J]
- Stowe R A,Champlain A D,Mayer A E H J.Modelling combustor performance of a ducted rocket[R].AIAA 2000-3728. 陈林泉;毛根旺;霍东兴;等.;燃气喷射方式对冲压发动机补燃室掺混效果的影响[J]
- In this paper, the theory of minitype Solid Ducted Rocket with shot is researche nd analyzed. 本文研究和分析了炮射小型固体火箭冲压发动机的工作原理。
- It would be of great reference value for development of air-to-air missile propelled by integral solid ducted rocket. 对我国发展采用整体式固冲发动机的空空导弹具有重要的参考价值。
- Mayer A E H J,Stowe R A.Experimental study into mixing in a solid fuel ducted rocket combustion chamber[R].AIAA 2000-3346. 余勇;陈小前;等.;三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟[J]
- Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails. 四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。
- 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。
- Rocket motors have many advantages over other forms of propulsion. 火箭发动机比其他推进器有许多优点。
- Mayer A E H J,Stowe R A. Experimental Study Into Mixing in a Solid Fuel Ducted Rocket Combustion Chamber[R]. AIAA Paper 2000-3346. 张炜;夏智勋;姜春林;等.;新型非壅塞式固体火箭冲压发动机试验研究[J]
- There is a rocket motor on the satellite by which the direction of the satellite can be changed if necessary. 在卫星上还有一个火箭马达,必要时可以用它来改变卫星的方向。
- According to the requirement of pasty propellant rocket motor, a composite plasma igniting plan was adopted. 摘要根据膏体推进剂火箭发动机。
- 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。
