| 1. | Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails .
四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。 |
| 2. | Vibration test method for solid rocket motors
固体火箭发动机振动试验方法 |
| 3. | Web - based integrated design platform for solid rocket motor
的固体火箭发动机集成设计平台 |
| 4. | Railway transportation test method for solid rocket motors
固体火箭发动机铁路运输试验方法 |
| 5. | Shock test method for solid rocket motors
固体火箭发动机冲击试验方法 |
| 6. | Calculation of nozzle efficiency for solid rocket motor
固体火箭发动机燃烧室喷管一体化网格生成 |
| 7. | Uncertainty optimization design of solid rocket motor grain
固体火箭发动机装药不确定性优化设计 |
| 8. | Analysis of nozzleless solid propellant rocket motor performance
无喷管固体火箭发动机内弹道计算 |
| 9. | Application study of plug nozzles for solid rocket motors
固体火箭发动机柔性接头贮存老化可靠度研究 |
| 10. | Critical techniques in development of large - size solid rocket motors
大型固体火箭发动机研制的关键技术 |
