CHINESE JOURNAL OF ENERGETIC MATERIALS
+Advanced Search

Simulation on Influence of Residual Rocket Motor Propellant on Warhead Damage Effect
Author:
Affiliation:

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

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
    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.

    Reference
    Related
    Cited by
Article Metrics
  • PDF:
  • HTML:
  • Abstract:
  • Cited by:
Get Citation

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.
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.

Cope
History
  • Received:August 31,2011
  • Revised:November 14,2011
  • Adopted:November 02,2011
  • Online: February 22,2012
  • Published: