Design Considerations of RBCC-powered Vehicle

被引：0
|
作者：
Lv Xiang [1 ]
He Guoqiang [1 ]
Liu Peijin [1 ]
Liu Yang [1 ]
机构：
[1] Northwestern Polytech Univ, Natl Key Lab Combust Flow & Thermostruct, Xian 710072, Peoples R China
来源：
PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2 | 2010年
关键词：
rocket based combined cycle; system design; hypersonic vehicle; experimental investigation; mode transition; thermal choke;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
RBCC has recentlyreceived increased attention for the next generation reusable launch vehicles and hypersonic cruise vehicles. System design of RBCC-powered vehicle is carried out in Northwestern Polytechnical University, accompanied with experimental investigation. Both system requirements evaluation and performance analysis model is established, adopted by the system design and optimization program. Combustion management techniques for high combustion efficiency and engine performance is studied on the direct connect test facility, under the consideration of fuel injection, variable geometry, and thermal choke control. Mode transition is investigated with both analytical and experimental means, concluding several key techniques. Detailed design considerations of RBCC-powered vehicle is discussed, proposing the further development steps for RBCC.
引用
收藏
页码：1060 / 1063
页数：4
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