| 1. | Safety rules for hoisting of liquid rocket engine
液体火箭发动机吊装安全规定 |
| 2. | Bipropellant liquid rocket motor
二元推进剂液体火箭发动机 |
| 3. | Propositional logic - based method of liquid rocket engine fault diagnosis
液体火箭发动机故障诊断的命题逻辑方法 |
| 4. | Study on boiling heat transfer enhancement of forced liquid nitrogen flow in lunate narrow channel
低温液体火箭发动机循环预冷模拟试验 |
| 5. | The gas - phase inlet , the outlet of the reflux pipe is at above the liquid surface in the cryogenic tank , is presented
得出了循环预冷技术在低温液体火箭发动机预冷程序中可以采用的结论。 |
| 6. | In this paper , the characteristics of tripropellant rocket engine was studied in two different ways : experiment and simulation
本文从实验、仿真两个方面对三组元液体火箭发动机推力室的工作过程进行了研究。 |
| 7. | The fault of liquid rocket engine in the starting - up and shutdown process could be detected by judging whether the rules were valid or not
根据液体火箭发动机工作时,相应参数之间的关联关系是否有效,来检测液体火箭发动机的故障。 |
| 8. | Lacking of fault samples is a knotty problem in the fault detection of complex systems such as liquid - propellant rocket engines ( lre )
在对类似于液体火箭发动机这种复杂系统的故障检测过程中,一个非常棘手的问题是缺乏故障类样本。 |
| 9. | For liquid propellant rocket engine , it is an important condition for effective combustion that propellant be evaporated and mixed quickly
在液体火箭发动机中，推进剂组元迅速而高效的气化和混和是产生高质量燃烧所必须的重要条件。 |
| 10. | Owing to the dissimilar combustion mode , their working process is different form that of solid rocket motors and the liquid rocket engines
由于氧化剂和燃料的燃烧方式不同，固液火箭发动机工作过程和液体火箭发动机及固体火箭发动机有很大的区别。 |
