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1)  solid rocket ramjet
固体火箭冲压发动机
1.
Quick-forecasting algorithm for performance of solid rocket ramjet;
固体火箭冲压发动机性能快速预估算法
2.
Some technological problems of solid rocket ramjet;
固体火箭冲压发动机的若干技术问题
3.
Experimental study on solid rocket ramjet with central air-inlet mode;
中心进气式固体火箭冲压发动机试验研究
2)  solid ducted rocket
固体火箭冲压发动机
1.
Modeling and simulation on the gas generator and gas control valve of solid ducted rockets;
固体火箭冲压发动机燃气发生器及燃气流量调节阀建模及仿真
2.
Three dimension numerical simulation on air inlet of solid ducted rocket;
固体火箭冲压发动机进气道三维数值模拟
3.
Dynamic modeling and model reduction order of controllable flow solid ducted rockets;
燃气流量可控的固体火箭冲压发动机动态建模及模型降阶(英文)
3)  ducted rocket motor
固体火箭冲压发动机
1.
There are a variety of influential factors to the combustion efficiency of secondary chamber of boron-based propellant ducted rocket motor,which are difficult to be expressed accurately by analytical functions.
影响含硼推进剂固体火箭冲压发动机补燃室燃烧效率的因素很多,且各因素对燃烧效率的影响很难用精确的解析函数式来表示。
4)  solid ducted rocket motor
固体火箭冲压发动机
1.
Erosion test of the insulation in the ramjet combustor of solid ducted rocket motors;
固体火箭冲压发动机补燃室绝热层烧蚀试验研究
2.
The 3D reaction flow field in the afterburning chamber of solid ducted rocket motor with binary dual-underside inlet mode was numerically simulated by means of RNG κ-ε turbulence model and one step eddy-dissipation combustion model.
采用RNGκ-ε湍流模型及单步涡扩散燃烧模型,对二元双下侧进气式固体火箭冲压发动机补燃室内三维反应流场进行了数值模拟,得到了补燃室二次燃烧效率的变化趋势。
3.
By direct-conncted simulation calculation,the effects of common heater fuel (hydrogen,kerosene,methane and alcohol) on performance of solid ducted rocket motor with low-oxygen boron-based propellant were investigated.
通过直连模拟计算,研究了常用加热器燃料(氢气、煤油、甲烷和酒精等)对含硼贫氧推进剂固体火箭冲压发动机性能的影响。
5)  Solid liquid rocket ramjet engine
固液火箭冲压发动机
6)  Integral solide propellant rocket ramjet engine
整体式固体火箭冲压发动机
补充资料:固体火箭发动机静止实验
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性质:是指将装有一定质量推进剂的待测发动机,固定在地面静止试验台上进行的点火试验。静止试验主要测试压强、推力、比冲、测向分力、发动机各构件的应力、壁温和流量等参数。通过实验评定推进剂的性能以及发动机结构和性能。在火箭发动机研制、定型和生产验收等不同阶段,都要进行静止实验。 

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