节点文献

CMDB推进剂RDX填料表面包覆对其机械感度和力学性能的影响

Influence of surface coating of RDX fillers on mechanical sensitivity and properties of CMDB propellant

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 安崇伟宋小兰郭效德王毅阎斌李凤生

【Author】 AN Chong-wei1,SONG Xiao-lan1,GUO Xiao-de1,WANG Yi1,YAN Bin2,LI Feng-sheng1 (1.National Special Superfine Powder Engineering Research Center,Nanjing University of Science & Technology,Nanjing 210094,China;2.Shanxi North Xing′an Chemical Industry Co.LTD,Taiyuan 030008,China)

【机构】 南京理工大学国家特种超细粉体工程技术研究中心山西北方兴安化学工业有限公司南京理工大学国家特种超细粉体工程技术研究中心 南京210094南京210094太原030008

【摘要】 为了改善RDX-CMDB推进剂的安全性能和力学性能,用一种含能高分子材料(记为HP-1)和一种胺类物质(记为AM)对RDX填料进行了表面包覆。用SEM和XPS对包覆样品的包覆效果进行了表征,对包覆前后RDX样品的撞击感度、摩擦感度及CMDB推进剂的机械感度和力学性能进行了测试和对比。结果表明,单独用HP-1包覆的样品机械感度没有明显变化;而随着AM用量的增加,样品的摩擦感度和撞击感度都有下降的趋势,当HP-1和AM的含量分别为1%和0.5%时,样品的特性落高升高了约17 cm,摩擦爆炸概率由92%降到58%。通过对RDX填料进行包覆,CMDB推进剂的撞击感度没有明显变化,而摩擦感度由58%降到4%,各个温度下的力学性能也得到了很大改善。

【Abstract】 In order to improve safe and mechanical properties of the RDX-CMDB propellants,RDX fillers were coated with a kind of energetic high polymer(marked as HP-1) and a kind of amine material(marked as AM).The coated samples were characterized by means of SEM and XPS.The mechanical sensitivity of pre-and post-coated RDX samples was measured and contrasted,meanwhile the mechanical sensitivity and properties of CMDB propellants made with pre-and post-coated RDX were investigated respectively.The results indicate that the mechanical sensitivity of the sample merely coated with HP-1 varies scarcely,but the impact and friction sensitivity of samples decreases with the increase of the content of AM.When the content of HP-1 and AM are up to 1% and 0.5% respectively,the special height of the coated sample is higher about 17 cm than that of pure RDX,and the friction explosive probability reduces from 92% to 58%.with surface-coating RDX fillers,the impact sensitivity of CMDB propellant doesn’t vary obviously,but its friction sensitivity reduces from 58% to 4%,and the mechanical properties are greatly improved at various temperatures.

【基金】 国家自然科学基金资助项目(5060202450306008)
  • 【文献出处】 固体火箭技术 ,Journal of Solid Rocket Technology , 编辑部邮箱 ,2007年06期
  • 【分类号】V51
  • 【被引频次】25
  • 【下载频次】265
节点文献中: 

本文链接的文献网络图示:

本文的引文网络