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动能火箭弹定深技术
引用本文:杨东来,张有龙,李昊. 动能火箭弹定深技术[J]. 爆炸与冲击, 2009, 29(4): 439-443. DOI: 10.11883/1001-1455(2009)04-0439-05
作者姓名:杨东来  张有龙  李昊
作者单位:总装备部工程兵科研一所,江苏,无锡,214035;总装备部工程兵科研一所,江苏,无锡,214035;总装备部工程兵科研一所,江苏,无锡,214035
摘    要:根据某火箭破障弹的性能特点,设计了动能侵彻战斗部和机械定深发火机构,使其可根据目标的强度和厚度控制战斗部在最佳深度处爆炸,以发挥战斗部的爆破威力。理论和试验证明所设计的动能火箭弹结构合理可行。

关 键 词:爆炸力学  火箭破障弹  机械定深发火机构  战斗部

Adaptive breaching-depth control techniques for a new obstacle-breaching rocket projectile
YANG Dong-lai,ZHANG You-long,LI Hao. Adaptive breaching-depth control techniques for a new obstacle-breaching rocket projectile[J]. Explosion and Shock Waves, 2009, 29(4): 439-443. DOI: 10.11883/1001-1455(2009)04-0439-05
Authors:YANG Dong-lai  ZHANG You-long  LI Hao
Affiliation:1.The Frist Engineers Scientific Research Institute of the General Armaments Departments, wuxi 214035, Jiangsu, China
Abstract:A mechanical delay ignition device was designed on the basis of the characteristics of the investigated obstacle-breaching rocket projectile.The designed ignition device can check the obstacle-breaching power and make the kinetic energy penetrating warhead explode at the optimal depth.Theoretical and experimental results prove that the designed kinetic energy rock projectile structure is practicable.
Keywords:mechanics of explosion  obstacle-breaching rocket  mechanical delay ignition device  warhead  
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