气炮加载下炸药强爆轰驱动技术的初步实验研究

文尚刚; 赵锋; 王建; 赵玉刚; 翁继东; 王翔

doi:10.11858/gywlxb.2011.01.006

气炮加载下炸药强爆轰驱动技术的初步实验研究

doi: 10.11858/gywlxb.2011.01.006

中国工程物理研究院流体物理研究所，冲击波物理与爆轰物理国防科技重点实验室，四川绵阳 621900

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通讯作者:
文尚刚

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出版历程
- 收稿日期: 2010-02-20
- 修回日期: 2010-06-29
- 发布日期: 2011-02-15

Primary Experimental Study on Driving Technique of Strong Detonation Using Gas Gun

National Key Laboratory of Shock Wave and Detonation Physics, Institute of Fluid Physics, CAEP, Mianyang 621900, China

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Corresponding author: WEN Shang-Gang

摘要

摘要: 利用二级轻气炮进行了炸药强爆轰驱动超高速飞片技术的研究，采用多普勒探针系统（Doppler Pins System，简称DPS）对二级飞片的速度历史进行了测量。初步获得了在较高速度（大于5 km/s）一级飞片的作用下、二级飞片的速度增益情况，并基本掌握了强爆轰驱动技术与二级轻气炮发射技术有机结合的实验技术。初步实验结果表明，采用炸药强爆轰驱动技术可使二级飞片获得较高的速度增益。
- 气炮 /
- 炸药 /
- 强爆轰驱动 /
- 超高速飞片
Abstract: Using the loading technique of two-stage gas gun and the doppler pin system, the driving technique of strong detonation is studied. The velocity increment of the secondary flyer is obtained when the velocities of the first flyer surpass 5 km/s. The loading technique of two-stage gas gun and the driving technique of strong detonation are combined very well. The primary experimental results show that the velocity increment of the secondary flyer is considerably large if the two techniques are combined together.
- gas gun /
- explosive /
- strong detonation driving /
- hypervelocity flyer

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参考文献(11)

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