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- unchoked solid ducted rocket engine 非壅塞固体火箭冲压发动机
- 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。
- 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。
- 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
- The Optimum Intermediate Guidance Law of Missile Considering the Characteristic of Solid Ducted Rocket 考虑冲压发动机特性的导弹最优中制导律研究
- 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
- 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;
- solid ducted rocket motor 固体火箭冲压发动机
- Solid ducted rocket (SDR) 固体火箭冲压发动机
- ducted rocket engine 火箭冲压发动机
- solid ducted rocket 固体火箭冲压发动机
- 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。
- 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]
- 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。
- 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]
