RBCC和TBCC组合发动机在RLV上的应用  

Application of RBCC and TBCC engines to RLVs

作　　者：陈宏[1] 何国强[2] 

机构地区：[1]中国航天科技集团公司第四研究院第四十一所,陕西西安710025 [2]西北工业大学航天学院,陕西西安710072

出　　处：《火箭推进》2008年第3期39-43,共5页Journal of Rocket Propulsion

摘　　要：论述了吸气式组合发动机在新一代可重复使用运载器上的使用现状,分析了各种组合方案的优势和特点,着重介绍了RBCC、TBCC的应用对飞行器总体性能的影响,并提出了两种较优的飞行器组合结构方案。The application of combined airbreathing engines used for the next generation reusable launch vehicle （RLV） was presented. Two-Stage-To-Orbit RLV configurations using combined propulsion systems for both stages were described, and a comparison was made between RBCC and TBCC to analyze their effects on the general performances of RLV. Two recommended RLV configurations were shown consequently.

关 键 词：两相反应 燃烧室 有限速率 EDC PDF 燃烧模型 

分 类 号：V438[航空宇航科学与技术—航空宇航推进理论与工程]