固体火箭推进剂用燃烧催化剂研究新进展  

New Progress of Study on Combustion Catalysts used for Solid Rocket Propellants

作　　者：汪营磊[1] 赵凤起[1] 仪建华[1] 

机构地区：[1]西安近代化学研究所燃烧与爆炸技术重点实验室,陕西西安710065

出　　处：《火炸药学报》2012年第5期1-8,共8页Chinese Journal of Explosives & Propellants

基　　金：国家自然科学基金(No.21173163)

摘　　要：从纳米燃烧催化剂、含能催化剂和双金属燃烧催化剂三方面综述燃烧催化剂的研究新进展。总结了各类催化剂的特点和发展过程中的技术难题,指出燃烧催化剂的发展方向,如纳米催化剂的团聚抑制和催化机理、含能催化剂能量与感度的统一以及双金属催化剂的结构表征和含能化等。附参考文献55篇。The new progresses in the combustion catalysts, divided into three aspects which are nano-catalysts, energetic catalysts and bi-metal catalysts, were reviewed. The characteristics of different combustion catalysts and its technical problems under development were summarized, and the new insights on the development of combustion catalysts were pointed out, such as the anti-agglomeration and catalytic mechanisms of nano catalysts, the correlation of energy and sensitivity on energetic catalysts, structural analysis and energization of hi-metal catalysts with 55 references.

关 键 词：物理化学 纳米催化剂 含能催化剂 双金属催化剂 固体推进剂 

分 类 号：TJ55[兵器科学与技术—军事化学与烟火技术] V512[航空宇航科学与技术—航空宇航推进理论与工程]