液体火箭凝胶推进剂燃烧特性研究进展  

Progress in combustion characteristic research of liquid rocket gelled propellants

作　　者：丰松江[1] 何博[1] 聂万胜[1] 

机构地区：[1]装备指挥技术学院,北京101416

出　　处：《火箭推进》2009年第4期1-7,13,共8页Journal of Rocket Propulsion

基　　金：国家自然科学基金(50576105)

摘　　要：液体火箭凝胶推进剂燃烧特性是凝胶推进技术发展的关键问题之一。综述了液体火箭凝胶推进剂燃烧特性研究状况与进展,详细阐述了凝胶液滴燃烧机理,总结分析了凝胶推进剂燃烧特性三种试验研究方案和四种理论研究模型的特点,指出了研究凝胶推进剂燃烧特性的重要性并对进一步的研究工作提出建议。Combustion characteristic of liquid rocket gelled propellants is one of the key problems for development of gelled propulsion technology. Research and development of combustion characteristic of liquid rocket gelled propellants were summarized. The combustion mechanisms of gelled propellants droplets were introduced. The characteristics of three kinds of experimental schemes and four kinds of theoretical modes were summarized and analyzed respectively. The importance of the gelled propellants combustion characteristic research was addressed. In addition, some proposals were given based on the research work.

关 键 词：凝胶推进剂 燃烧 研究进展 

分 类 号：V434[航空宇航科学与技术—航空宇航推进理论与工程]