| 可延伸出口锥对推力向量控制系统稳定性的影响 |
| |
| 引用本文： | 何景轩.可延伸出口锥对推力向量控制系统稳定性的影响[J].固体火箭技术,1994,17(1):22-26. |
| |
| 作者姓名： | 何景轩 |
| |
| 作者单位： | 中国航天工业总公司四院四十一所 西安 |
| |
| 摘 要： | 介绍了喷管可延伸出口锥对大型固体火箭发动机推力向量控制系统稳定性的影响,并提出了改善其系统稳定性的措施。
|
| 关 键 词： | 喷管 火箭发动机 推力矢量控制 |
The Effects of the Extendible Exit Cone on Stability of the Thrust Vector Control System |
| |
| He Jingxuan.The Effects of the Extendible Exit Cone on Stability of the Thrust Vector Control System[J].Journal of Solid Rocket Technology,1994,17(1):22-26. |
| |
| Authors: | He Jingxuan |
| |
| Abstract: | The effects of the extendible exit cone on stability of the thrust vector control system of largescale solid rocket motor are presented and the measures for improving the system stability are suggested. |
| |
| Keywords: | Extension nozzle Rocket motor nozzle Thrust vector control Stability |
| 本文献已被 CNKI 维普 等数据库收录！ |
