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火箭发动机残余装药对战斗部毁伤效果影响的模拟研究

王宁 赵孝彬 王晨雪 田军

含能材料2011,Vol.19Issue(6):720-724,5.
含能材料2011,Vol.19Issue(6):720-724,5.DOI:10.3969/j.issn.1006-9941.2011.06.026

火箭发动机残余装药对战斗部毁伤效果影响的模拟研究

Simulation on Influence of Residual Rocket Motor Propellant on Warhead Damage Effect

王宁 1赵孝彬 1王晨雪 1田军1

作者信息

  • 1. 航天工业固体推进剂安全技术研究中心,湖北 襄樊 441003
  • 折叠

摘要

Abstract

The influence of solid propellant on warhead damage effect was studied by these quantitative parameters including lead cylinder compression value,lead block volume,shock wave overpressure and impulse. Influencing factors that effect lead cylinder compression value of warhead charge/propellant system was also discussed. The results show that four kinds of propellants all could enhance lead cylinder compression value of warhead charge/propellant system in different degrees. Contribution to lead cylinder compression value of warhead charge/ propellant system by four groups HTPB propellant is more than that by three groups HTPB propellant ( HTPB-3). Increased percentage of lead block volume is 81.4% and 54% ,respectively. When scaled distance ranges from 3.5 m· kg-1/3 to 12.5 m ? Kg-1/3,HTPB-3 contributes to shock wave overpressure TNT equivalence and impulse TNT equivalence of 1 kg PBXN/0.6 kg HTPB-3 system by an increase of 18.7% and 19.7%,respectively.

关键词

爆炸力学/推进剂残余装药/引爆技术/毁伤效果增益

Key words

mechanics of explosion/ residual propellant charge/ initiating technique/ damage effect gain

分类

军事科技

引用本文复制引用

王宁,赵孝彬,王晨雪,田军..火箭发动机残余装药对战斗部毁伤效果影响的模拟研究[J].含能材料,2011,19(6):720-724,5.

含能材料

OA北大核心CSCDCSTPCD

1006-9941

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