[1]苏晶,李军,陈怡,等.固体推进剂爆轰感度影响因素研究[J].固体火箭技术,2019,42(04):466-470.
 SU Jing,LI Jun,CHEN Yi,et al.Research on the influencing factors of detonation sensitivity of solid propellant[J].Journal of Solid Rocket Technology,2019,42(04):466-470.
点击复制

固体推进剂爆轰感度影响因素研究

参考文献/References:

[1]胥会祥,李兴文,赵凤起.纳米金属粉在火炸药中应用进展[J].含能材料,2011,19(2):232-239.XU Huixiang,LI Xingwen,ZHAO Fengqi.Progress in application of nano metal powder in fire explosives[J].Chinese Journal of Energetic Materials,2011,19(2):232-239.[2]Babaitsev I V,Kozak N V,Antipova F V.Calculating the detonation parameters of mixtures of hexogen and inert additives[J].Metallurgist,2007,51(7-8):401-404.[3]Victor V Odintsov,Vitaly L Pepekn.Comparative brisant characteristics of some classes of industrial emulsion explosives[J].Propellants,Explosives,Pyrotechnics,1996,21:295-302.[4]Voskoboinikov I M,Kotomin A A.Calculation of detonation parameters for explosive mixture with inert additions[J].Combustion,Explosion and Shock Waves,1985,21(5):93-97.[5]白春华,丁敬.固体推进剂在冲击波作用下化学反应过程的研究[J].兵工学报,1991,12(3):38-47.BAI Chunhua,DING Jing.Study on the chemical reaction process of solid propellant under the action of shock wave[J].Acta Armamentarii,1991,12(3):38-47.[6]郑波,袁鹏刚.验证板反射冲击波对固体推进剂冲击起爆影响的实验研究[J].固体火箭技术,2014,37(5):734-736.ZHENG Bo,YUAN Penggang.Experimental study on the effect of reflecting shock waves on the impact of solid popellant impact detonation[J].Journal of Solid Rocket Technology,2014,37(5):734-736.[7]黄明,李洪珍,徐容.高品质RDX的晶体特性及冲击波起爆特性[J].含能材料,2011,19(6):621-626.HUANG Ming,LI Hongzhen,XU Rong.Crystal properties and shock wave initiation characteristics of high quality RDX[J].Chinese Journal of Energetic Materials,2011,19(6):621-626.[8]MIL-STD-1751A.Safety and performance tests for the qualification of explosives[S].2001.[9]Irwin O R ,Roark G L ,Salzman P K .Large solid-propellant boosters explosives hazards study program[R].AD476617,1971.

相似文献/References:

[1]田四朋,唐国金,雷勇军,等.固体火箭发动机随机药柱结构分析参数的灵敏度研究[J].固体火箭技术,2008,(1):28.
[2]封锋,陈军,郑亚.基于能量特性配方设计专家系统的开发与实现[J].固体火箭技术,2009,(02):206.
[3]张伟,樊学忠,张腊莹,等.NEPE推进剂低温瞬态的粘弹特性[J].固体火箭技术,2009,(03):298.
[4]阳建红,刘朝丰,邓凯.固体推进剂的变角剪切力学试验研究[J].固体火箭技术,2009,(04):436.
[5]闫大庆,徐丹丹,师经国.固体推进剂粘合剂HTPE研究及其分子设计思想概述[J].固体火箭技术,2009,(06):644.
[6]李苗苗,汪越,郭效德,等.RDX/AMMO-BAMO推进剂燃烧模型[J].固体火箭技术,2009,(06):654.
[7]陈煜,刘云飞,夏吉东,等.键合剂对NEPE推进剂破坏趋势影响的实验定量研究[J].固体火箭技术,2010,(03):299.
[8]刘中兵,汪亮,胡春波.HTPB推进剂高压燃烧特性研究[J].固体火箭技术,2010,(03):302.
[9]段毅,刘宇,覃粒子,等.考虑两相表面反应的二硝酰胺铵点火研究[J].固体火箭技术,2010,(03):311.
[10]刘晶如,罗运军.固体推进剂用铝基复合材料的制备及性能[J].固体火箭技术,2010,(05):545.

更新日期/Last Update: 2019-08-29
PDF下载 分享