monopropellant信息详情
n.单一组分的喷气机燃料
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。
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系统重要组成部分。
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系统（包括结构部件如隔热框、催化床、喷管等）的传热模型。
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。
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。
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
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系统重要组成部分。
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仿真
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
The comparison between the solid bipropellant firing results and the monopropellant firing results appears to be quite good.