| 吸气式远程超声速防空导弹一体化外形设计的几个重大技术问题 |
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| 引用本文： | 李国雄.吸气式远程超声速防空导弹一体化外形设计的几个重大技术问题[J].现代防御技术,2002,30(2):29-34. |
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| 作者姓名： | 李国雄 |
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| 作者单位： | 中国航天科工集团公司二院二部,北京,100854 |
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| 摘 要： | 根据国外吸气式超声速战术导弹一体化外形设计取得的最新进展 ,着重分析了这类导弹外形设计的特点和技术关键 ,提出了吸气式远程超声速防空导弹一体化外形设计中应解决好的几个重大技术问题 ,以期引起各方对吸气式防空导弹总体设计中有关问题的关注和讨论 ,共同寻找解决这些技术问题的有效途径
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| 关 键 词： | 吸气式导弹 进气道 气动布局 一体化外形设计 |
| 文章编号： | 1009-086X(2002)02-0029-06 |
| 修稿时间： | 2001年9月5日 |
Several important technical questions in integrated configuration design of air-breathing long-range supersonic surface-to-air missiles |
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| LI Guo,xiong.Several important technical questions in integrated configuration design of air-breathing long-range supersonic surface-to-air missiles[J].Modern Defence Technology,2002,30(2):29-34. |
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| Authors: | LI Guo xiong |
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| Abstract: | According to the current progress of overseas integrated configuration design of air breathing supersonic missiles,characteristic and key points of configuration design of such missiles are analyzed,as well as several important technical questions are introduced in this paper.Purpose of this paper is to raise wide dis cussion and attention about the related issues in the design of air breathing surface to air missiles and to find out an efficient way of solution. |
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| Keywords: | Air breathing missile Inlet Aerodynamic configuration Integrated configuration design |
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