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弹炮间隙对火箭弹初始扰动的影响

EFFECTION ON INITIAL DISTURBANCE OF ROCKET BY CHINK BETWEEN ROCKET AND LAUNCHER

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【作者】 骆连珍徐明友姜慧春曹勇

【Author】 Luo Lianzhen ① Xu Mingyou ① Jiang Huichun ② Cao Yong ③ ①Power Eng. College, NUST, Nanjing, 210094 ②Tongchuang Group of Nanjing, Nanjing, 210094 ③Party School of Qixiaqu, Nanjing, 210046$$$$

【机构】 南京理工大学动力工程学院!南京210094南京同创集团!南京210004南京市栖霞区党校!南京210046

【摘要】 以螺旋导轨导旋的多管火箭发射系统为研究对象,考虑弹炮间隙对系统的影响,建立了弹炮耦合运动模型,分析了各种可能的膛内运动姿态,并着重研究了弹炮间隙的存在对膛内运动姿态和起始扰动结果的影响.

【Abstract】 In this paper Multiple Launchers Rocket System (MLRS) with helical railis is studied. The effect of chink between rocket and launchers is considerated. Model of motion including them two is established. Serval kinds of ways of motion in gun tube is analysed. The effect of rocket and ways of motion in gun tube is researched with varing chink between rocket and launchers.

  • 【文献出处】 弹道学报 ,JOURNAL OF BALLISTICS , 编辑部邮箱 ,1999年03期
  • 【分类号】TJ013
  • 【被引频次】12
  • 【下载频次】208
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