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| 固体火箭发动机推力大小调节技术的发展 | |
| 引用本文： | 徐温干.固体火箭发动机推力大小调节技术的发展[J].推进技术,1994,15(1):39-44. |
| 作者姓名： | 徐温干 |
| 作者单位： | 上海新风化工研究所 |
| 摘 要： | 对固体火箭发动机推力大小调节技术研究的必要性，发展的现状以及在型号上应用的情况作了综述与分析。指出了发展的趋势与方向。 |
| 关 键 词： | 固体推进剂 火箭发动机 可变推力 |
THE DEVELOPMENT FOR TECHNIQUE OF ADJUSTING THRUST OF SOLID ROCKET MOTOR |
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| Xu Wengan.THE DEVELOPMENT FOR TECHNIQUE OF ADJUSTING THRUST OF SOLID ROCKET MOTOR[J].Journal of Propulsion Technology,1994,15(1):39-44. | |
| Authors: | Xu Wengan |
| Institution: | Shanghai Xin Feng Chemical Engineering institute, Huzhou, 313022 |
| Abstract: | he necessity and present situation of research for adjusting the thrust of solid rocket motor and its application have been review. It also pointed out the further direction for the research. |
| Keywords: | Solid propellant rocket engine Variable thrust Controllable thrust rocket engine Restartable rocket engine impulse rocket engine |
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