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Remote Anti-missile Capability of Gun-launched Fuel-air-explosive Projectile


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Remote Anti-missile Capability of Gun-launched Fuel-air-explosive Projectile
CHEN Hong-binDU Zhong-huaCHEN Long-miaoCHEN Guang-song
School of Mechanical Engineering,NUST,Nanjing 210094,China
gun-launched fuel-air-explosive projectiles anti-missile capability impulse criterions mode analysiskill probabilities
To improve the remote anti-missile capability of the medium caliber gun,an anti-missile combat mode for the gun-launched single event fuel-air-explosive( SEFAE) projectile is put forward based on the ballistic characteristics,detonation features and the damage mechanism of the fuel-air- explosive(FAE) here. The shock wave damage criterions of FAE projectile and the high-explosive (HE)projectile are established considering target features,and the effective lethal area of the shock wave against the cruise-guide missile( CGM) is obtained. The kill probabilities of the gun-launched SEFAE projectile and HE projectile are simulated in long ranges. The results show that the impulse criterion is suitable for evaluating the damaging efficiency of shock waves of the low dose SEFAE projectile against the CGM projectile and the gun-launched FAE projectile possesses higher remote anti-missile capabilities than HE projectile.


[1]Borisov A A. Fuel-air explosives[R]. Moscow,Russian: Institute of Chemical Physics, Russian Academy of Sciences,1994.
[2] 高洪泉,卢芳云,王少龙,等. 云爆弹结构对爆炸威 力影响规律的试验研究[ J]. 弹道学报,2010,22 (4):58-61. Gao Hongquan,Lu Fangyun,Wang Shaolong,et al. Ex- perimental study about influence of SEFAE device structure on SEFAE damage-power [ J]. Journal of Ballistic,2010,22(4):58-61.
[3] 黄来法. 温压药剂冲击波效应研究[D]. 南京:南京 理工大学机械工程学院,2008.
[4] 张鹏,朱平安,马翰宇,等. 炮射云爆战斗部二次起 爆时间的试验研究[ J]. 火炸药学报,2008,31(5): 55-58. Zhang Peng,Zhu Pingan,Ma Hanyu,et al. Experimental study on the initiation time of twice-detonating gun- launched FAE warhead [ J ]. Chinese Journal of Explosives and Propellants,2008,31(5):55-58.
[5] 郭振汉,钟宜兴,刘占锋. 122mm 火箭云爆弹射击误 差分析[J]. 弹道学报,2005,17(3):85-87. Guo Zhenhan,Zhong Yixing,Liu Zhanfeng. Analysis in firing error of 122mm fuel-air-explosive rocket [ J]. Journal of Ballistics,2005,17(3):85-87.
[6] 惠君明,刘荣海,彭金华,等. 燃料空气炸药威力的 评价方法[J]. 含能材料,1996,4(3):123-128. Hui Junming, Liu Ronghai, Peng Jinhua, et al. Evaluation method on power of fuel air explosive[ J]. Energetic Materials,1996,4(3):123-128.
[7] 王儒策. 弹丸终点效应[M]. 北京:北京理工大学出 版社,1993.
[8] 曾凡军. 某型防空火箭武器系统打击巡航导弹效能 分析[D]. 南京:南京理工大学机械工程学院,2009.
[9] 宗士增,钱林方,陈龙淼. 某轻型车载火炮架体在后 坐阻力作用下的响应分析[J]. 南京理工大学学报, 2007,31(6):727-730. Zong Shizeng,Qian Linfang,Chen Longmiao. Response analysis for carriage of truck-mounted howitzer under recoil resistance[ J]. Journal of Nanjing University of Science and Technology,2007,31(6):727-730.
[10] 宋志东,李运华,周伦. 壳体对云爆弹药燃料抛撒影 响的仿真分析[ J]. 系统仿真学报,2007,19(24): 5868-5870. Song Zhidong, Li Yunhua, Zhou Lun. Simulation analysis on effect of shell to spill of liquid fuel of FAE [J]. Journal of System Simulation, 2007, 19 ( 24): 5868-5870.


Last Update: 2012-11-26