| 临近空间动能武器弹道特性分析 |
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| 引用本文： | 李桢,李海阳,雍恩米.临近空间动能武器弹道特性分析[J].弹箭与制导学报,2009,29(3). |
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| 作者姓名： | 李桢 李海阳 雍恩米 |
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| 作者单位： | 国防科学技术大学航天与材料工程学院,长沙,410073 |
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| 摘 要： | 提出了用飞艇搭载动能武器,从临近空间远程打击各类目标的作战方案.建立了考虑地球旋转的射弹动力学模型,针对多种不同初始条件进行了弹道特性分析.结果表明将动能武器系统布置于临近空间的发射平台大大提高了其射程.
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| 关 键 词： | 临近空间 动能武器 弹道特性 |
The Analysis of Trajectory Characteristics of Near Space Kinetic Weapon |
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| LI Zhen,LI Haiyang,YONG Enmi.The Analysis of Trajectory Characteristics of Near Space Kinetic Weapon[J].Journal of Projectiles Rockets Missiles and Guidance,2009,29(3). |
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| Authors: | LI Zhen LI Haiyang YONG Enmi |
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| Affiliation: | LI Zhen,LI Haiyang,YONG Enmi(College of Aerospace , Material Engineering,NUDT,Changsha 410073,China) |
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| Abstract: | A scheme of striking various targlts by kinetic-energy weapon on airship in near space was put forward.Considering the rotation of the Earth,a dynamic model was established,and trajectory characteristics were analyzed under different initial conditions.The results indicate that the deployment of kinetic-energy weapon to near space launch platform will enhance the range. |
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| Keywords: | near space kinetic-energy weapons trajectory characteristic |
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