| 超声速导弹燃气舵系统设计研究 |
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| 作者单位： | 国防科技大学，北京机电工程研究所 |
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| 摘 要： | 以超声速导弹为对象,初步研究了燃气舵系统的设计.分析了燃气舵的气动布局以及在喷管上的安装位置对舵面效率的影响.在此基础上,结合助推器的性能参数,借助工程方法,对燃气舵的气动外形进行了设计.
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| 关 键 词： | 超声速导弹 燃气舵 气动外形 工程方法 |
Investigation into the Jet Vane System of Supersonic Missile |
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| Xue Kai. Investigation into the Jet Vane System of Supersonic Missile[J]. Tactical Missile Technology, 2008, 0(6) |
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| Authors: | Xue Kai |
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| Abstract: | The design of jet vane system is investigated preliminarily,which is based upon a supersonic missile.The efficiency of jet vane is analyzed,which can be influenced by both aerodynamic layout of jet vane and its setting position on the booster nozzle.The aerodynamic configuration of jet vane is designed preliminarily with the help of engineering method,which is combined with the performance parameters of roll booster. |
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| Keywords: | supersonic missile jet vane aerodynamic configuration engineering method |
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