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- unchoked solid ducted rocket engine 非壅塞固体火箭冲压发动机
- Study of the Unchoked Ducted Rocket Engine and Fuel-Rich Propellant 非壅塞固体火箭冲压发动机及其贫氧推进剂
- Keywords Integral rocket ramjet;Ducted rocket engine;Flow control;Oxygen poor fuel rich propellant; 整体式火箭冲压发动机;冲压火箭发动机;流量控制;贫氧富燃料推进剂;
- ducted rocket engine 火箭冲压发动机
- solid ducted rocket engine 固体火箭冲压发动机
- 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。
- For one thing, they simplify the design of a rocket engine. 首先,它们可以简化火箭发动机的设计。
- The rocket engine carries with it the oxygen of its own . 火箭发动机自带氧气。
- Mo nozzle for the rocket engine nozzle professional. 钼喷嘴专业用于火箭发动机喷嘴。
- Armstrong and Aldrin fired the lander rocket engine. 阿姆斯特朗和奥尔德林点燃了登月舱的火箭发动机。
- 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。
- Unlike a rocket engine, the jet engine, as you konw, is an "air breather" . 正如你们所知道的,这种喷气发动机与火箭发动机不同:它是“空气喷气发动机。”
- 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。
- Unlike a rocket engine, the jet engine, as you know, is an "air breather". 正如你们所知道的,这种喷气发动机与火箭发动机不同:它是“空气喷气发动机”。
- 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]
- The leak of Liquid Rocket Engine (LRE) is very common and dangerous. 液体火箭发动机的泄漏是常见和极其危险的故障。
- 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。
- 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]