模型与真实高氯酸铵/硝胺推进剂燃烧转爆轰的比较  

THE COMPARISON OF DEFLAGRATION TO DETONATION TRANSITION BETWEEN MODEL AND REAL AMMONIUM PERCHLORATE/NITRAMINE PROPELLANT

作　　者：刘德辉[1] 潘孟春[1] 彭培根[1] 王振芳[1] 

机构地区：[1]国防科技大学

出　　处：《推进技术》1992年第5期74-77,43,共5页Journal of Propulsion Technology

摘　　要：详细地研究了硝胺炸药(RDX、HMX)对模型与真实高氯酸铵/硝胺推进剂DDT的影响。实验结果表明,硝胺炸药对上述两种推进剂的DDT具有不同的影响规律,作者分析了产生这种现象的原因。In this paper, the effects of nitramine explosives (RDX, HMX)on the DDT of model and real ammonium perchlorate/nitramine pro-pellants are studied in detail, Experimental results show that the feature of the effect of nitramine explosive on the DDT of model propellent is different from that of real propellant. The cause of the mentioned above phenomenon is also analysed in the paper.

关 键 词：固体推进剂 爆燃 爆轰 高氯酸铵 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]