ducted rocket信息详情
导管火箭；火箭冲压发动机
rocket───v.迅速增加；飞速移动；迅速成功；用火箭武器攻击；用火箭运载；n.火箭；火箭武器；烟花；芝麻菜；（非正式）严厉斥责
carrier rocket───n.运载火箭
rocket fuel───火箭燃料
rocket launch───火箭发射
elytra rocket───甲状腺火箭
shadow rocket───影子火箭
rocket queen───火箭皇后
publisher rocket───火箭出版社
rocket scientist───火箭专家；股市分析高手；行家；<俚>穿梭于金融市场的行家
characterization of the combustion properties of the aluminum? Magnesium fuel? Rich propellant for unchoked ducted rocket was studied.───研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
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。
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。
In this paper, the theory of minitype Solid Ducted Rocket with shot is research e 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。
At first, the thermodynamic calculation of Solid Ducted Rocket is researched.───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。
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
Study on Burning Rate of Boron Particles in Secondary Chamber of Ducted Rocket under Forced Convection Conditions───固冲发动机补燃室内强迫对流条件下硼颗粒燃烧速率研究
A Numerical Study on Ignition and Combustion of Boron Particles in the Flowfield of a Ducted Rocket Secondary Combustor───固冲发动机补燃室内硼颗粒点火和燃烧数值研究
An experimental method for simulating oxygen-rich condition in afterburning chamber of solid ducted rocket(SDR) was developed for insulation ablation investigation.