CHINESE JOURNAL OF ENERGETIC MATERIALS
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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
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航天工业固体推进剂安全技术研究中心,航天工业固体推进剂安全技术研究中心,航天工业固体推进剂安全技术研究中心,航天工业固体推进剂安全技术研究中心

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王宁(1982-),男,工程师,主要从事固体推进剂安全性能研究。e-mail: sdwn8211@163.com

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Simulation on Influence of Residual Rocket Motor Propellant on Warhead Damage Effect
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Aerospace industry research center of composite solid propellant safety technology,Aerospace industry research center of composite solid propellant safety technology,Aerospace industry research center of composite solid propellant safety technology,Aerospace industry research center of composite solid propellant safety technology

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    摘要:

    利用铅柱压缩量、铅壔扩孔值和冲击波超压与冲量等参数定量研究了推进剂残余装药对战斗部爆炸毁伤效果的影响,并探讨了影响战斗部装药/推进剂体系铅柱压缩量的因素。试验结果表明,四种推进剂的存在对战斗部装药/推进剂体系的铅柱压缩量均有不同程度的增益作用。HTPB四组元推进剂对战斗部装药/推进剂体系的铅柱压缩量和铅壔扩孔值的贡献量要高于HTPB三组元推进剂(HTPB-3),其铅壔扩孔值的增益量分别为81.4%和54%。比例距离范围为3.5~12.5 m·kg-1/3时,HTPB-3对1 kg战斗部装药PBXN/0.6 kg HTPB-3体系的超压TNT当量和冲量TNT当量分别贡献了18.7%和19.7%。

    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.

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王宁,赵孝彬,王晨雪,等.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. DOI:10.3969/j. issn.1006-9941.2011.06.026.
WANG Ning, ZHAO Xiao-bin, WANG Chen-xue, et al. Simulation on Influence of Residual Rocket Motor Propellant on Warhead Damage Effect[J]. Chinese Journal of Energetic Materials, 2011, 19(6):720-724. DOI:10.3969/j. issn.1006-9941.2011.06.026.

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  • 收稿日期: 2011-08-31
  • 最后修改日期: 2011-11-14
  • 录用日期: 2011-11-02
  • 在线发布日期: 2012-02-22
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