| RBCC和TBCC组合发动机在RLV上的应用 |
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| 引用本文： | 陈宏,何国强. RBCC和TBCC组合发动机在RLV上的应用[J]. 火箭推进, 2008, 34(3): 39-43 |
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| 作者姓名： | 陈宏 何国强 |
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| 作者单位： | 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 |
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| 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。
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| 关 键 词： | 两相反应 燃烧室 有限速率 EDC PDF 燃烧模型 |
Application of RBCC and TBCC engines to RLVs |
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| Chen Hong,He Guoqiang. Application of RBCC and TBCC engines to RLVs[J]. Journal of Rocket Propulsion, 2008, 34(3): 39-43 |
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| Authors: | Chen Hong He Guoqiang |
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| Affiliation: | Chen Hong1,He Guoqiang2 (1 The 41st Institute of the Fourth Academy of CASC,National Key Lab of Combustion,Flow , Thermo-Structure,Xi'an 710025,China,2 College of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China) |
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| Abstract: | 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. |
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| Keywords: | two-phase reacting flow combustion chamber finite rate EDC PDF combustion model |
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