脱壳弹穿甲后效及引燃性能的试验研究  

Experimental Study on APDS Penetration After-Effect and Ignition Performance

作　　者：张松松 陈英 薛建锋[2] 

机构地区：[1]九江国科远大机电有限公司,江西九江330400 [2]南京理工大学机械工程学院,南京210094

出　　处：《兵器装备工程学报》2017年第1期40-43,46,共5页Journal of Ordnance Equipment Engineering

摘　　要：利用25高炮发射进行了穿甲试验、毁伤后效试验及引燃试验,选用试验弹模拟1 000 m着速,依次射击25 mm/60°均质装甲板、飞行器设备舱模拟靶、武装直升机有防护驾驶舱模拟靶、地面装甲车燃油箱模拟靶,得到了对不同目标靶试验后的弹体穿甲威力及后效性能和引燃燃油性能相关数据,对脱壳弹的结构设计和毁伤评估有一定参考价值。In order to study penetrating power and aftereffect and diesel performance of missile,the experiments were carried out using 25 mm gun battle. The velocities of projectiles were about 1000 m/s,which shoots 25 mm/60° of homogeneous armor plate,and aircraft equipment module simulation target,and armed helicopter has protective cockpit simulation target,and ground armored vehicle fuel tank simulation target. The experimental results of different targets were obtained,which provides a certain reference value for the structure design of the APDS.

关 键 词：脱壳弹 穿甲 毁伤后效 引燃 模拟靶 

分 类 号：TJ391.9[兵器科学与技术—火炮、自动武器与弹药工程]