| 洲际弹道导弹大气层外弹道设计 |
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| 引用本文： | 唐明亮,谷良贤.洲际弹道导弹大气层外弹道设计[J].飞行力学,2006,24(4):57-60. |
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| 作者姓名： | 唐明亮 谷良贤 |
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| 作者单位： | 西北工业大学,航天学院,陕西,西安,710072 |
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| 摘 要： | 为了克服洲际导弹弹道常规设计方案的缺点,提高快速性,提出了一种新的弹道方案:弹头在大气层外飞行时,增添加速环绕段和下降段。通过比较传统方案和新方案的仿真结果,总结了新方案的优缺点。
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| 关 键 词： | 洲际弹道导弹 弹道设计 突防能力 |
| 文章编号： | 1002-0853(2006)04-0057-04 |
| 收稿时间： | 2005-10-27 |
| 修稿时间： | 2006-09-18 |
Extra-atmospheric Trajectory Design of an Intercontinental Ballistic Missile |
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| TANG Ming-liang,GU Liang-xian.Extra-atmospheric Trajectory Design of an Intercontinental Ballistic Missile[J].Flight Dynamics,2006,24(4):57-60. |
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| Authors: | TANG Ming-liang GU Liang-xian |
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| Abstract: | In order to overcome the defects in traditional method of trajectory design for ICBM.This paper presents a new method: adding accelerated encircling phase and swooping phase in extra-atmospheric flight.The advantages and disadvantages of new method are summarized by contrasting trajectory simulation results of the traditional method and the new one. |
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| Keywords: | ICBM trajectory design penetration ability |
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