| 弹管间隙对多管火箭密集度的影响 |
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| 引用本文： | 王国平,芮筱亭.弹管间隙对多管火箭密集度的影响[J].弹道学报,2003,15(4):27-31. |
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| 作者姓名： | 王国平 芮筱亭 |
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| 作者单位： | 南京理工大学动力工程学院,南京,210094 |
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| 摘 要： | 应用发射动力学理论，建立了考虑弹管间隙的多管火箭发射动力学方程．对某多管火箭武器弹管间隙与起始扰动及密集度进行了仿真，分析了弹管间隙与起始扰动及射击密集度的关系，为提高多管火箭射击密集度提供了一种思路。
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| 关 键 词： | 多管火箭 弹管间隙 起始扰动 密集度 |
| 修稿时间： | 2003年4月13日 |
INFLUENCE OF WINDAGE OF TUBULAR LAUNCHER TO DISPERSION OF MLRS |
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| Wang Guoping,Rui Xiaoting.INFLUENCE OF WINDAGE OF TUBULAR LAUNCHER TO DISPERSION OF MLRS[J].Journal of Ballistics,2003,15(4):27-31. |
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| Authors: | Wang Guoping Rui Xiaoting |
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| Abstract: | The launching dynamic equeations considering windage of tubular launcher was established by using launching dynamics theory. The windage of tubular launcher, initial disturbance and dispersion of a Multiple Launch Rocket System (MLRS) were simulated. The relations among windage of tubular launcher, initial disturbance and dispersion were analyzed. The thought to improve the dispersion was presented. |
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| Keywords: | multiple launch rocket system windage of tubular launcher initial disturbance dispersion |
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