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n.单一组分的喷气机燃料
1、Based on a thermal model of monopropellant thrust chamber system including its components such as adiabatic frame, catalyst bed, nozzle etc.───建立了单组元发动机推力室XiTong（包括结构部件如隔热框、催化床、喷管等）的传热模型。
2、Numerical simulation for temperature in a monopropellant thrust chamber on the orbit───单组元发动机推力室在轨温度数值FangZhen
3、The ignition and combustion properties of liquid monopropellant LP1846 droplet have been investigated in hot convection ambience.───研究单元液体推进剂LP1846液滴在高温对流环境中着火、燃烧的特性。
4、thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system───单组元肼分解发动机的热控制与热分析是空间推进XiTong重要组成部分。
5、The comparison between the solid bipropellant firing results and the monopropellant firing results appears to be quite good.───固体二元推进剂和单元推进剂的点火试验结果是很相近的。
6、Measurement of Linear Burning Rate of Liquid Monopropellant in High Pressures───单元液体发射药高压线燃速测定
7、The research emphasis is restartable nitrous oxide monopropellant thruster suitable for keeping the position and phase of small satellite.───研究重点是可多次启动的一氧化二氮单元推进剂推力室，适用于小卫星的位置保持和相位保持。
8、Temperature Distribution Measurement of High Energetic Monopropellant by Spectroscopic Diagnostic Technology───用光谱诊断技术测定高能单元推进剂的温度分布
9、Thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system.───单组元肼分解发动机的热控制与热分析是空间推进XiTong重要组成部分。
1、The comparison between the solid bipropellant firing results and the monopropellant firing results appears to be quite good.