Influence of eztended-range engine parameters on trajectory characteristics of terminal guidance projectile

摘要：

Based on ballistic model of terminal Guidance projectile, adopting calculation technology, the influence of main parameters of engine on trajectory is analyzed systemically. The main parameters of engine include engine ignition time, work time and engine average propulsive force. A series of data of nominal trajectorys falling range, falling velocity, falling angle are obtained. The conclusions lay foundation for further whole ballistic characteristics research have important guidance significance for engine design, structure parameters optimization, weapon system development, accuracy of shooting.

关键词： terminal-guidance engine parameter ballistic

作者: Song Wei-dong Lu Fei Zhao Qing-lan Deng Fu-ping

作者单位: Shijiazhuang Mechanical Engineering College, Shijiazhuang 050003, China Beijing Military Delegation Office,Beijing, 100000, China Ammunition and Missile Department, WuHan Ordnance N.C.O Academy of PLA, WuHan, 430000, P.R.China

会议类型: 国际会议

会议名称: 第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)

会议地点: 重庆

会议语种:英文

页码: 888-890

在线出版日期: 2009-08-01（万方平台首次上网日期，不代表论文的发表时间）