火箭冲压组合动力研究进展

Ya Jun Wang, Guo Qiang He, Fei Qin, Xiang Geng Wei, Duo Zhang

科研成果: 期刊稿件文献综述同行评审

14 引用 (Scopus)

摘要

The research status and development roadmap of the rocket based combined cycle (RBCC) engines both at home and abroad are summarized, and the main research plans and important achievements of each country are expounded. The research progress and achievements of the RBCC engine in Northwestern Polytechnical University are systematically summarized. After nearly two decades of development, the research including the theoretical analysis and principle verification, component design and testing, and small-scaled ground engine integration and verification is completed. A number of key technologies such as wide operating range full-path design, flame stability and high-efficiency combustion during wide incoming flow condition, as well as mode transition, are preliminarily mastered, and the basis for conducting flight demonstration verification is already in place.

投稿的翻译标题Research Progress of Rocket Based Combined Cycle Engines
源语言繁体中文
页(从-至)1125-1133
页数9
期刊Yuhang Xuebao/Journal of Astronautics
40
10
DOI
出版状态已出版 - 30 10月 2019

关键词

  • Key technology
  • Research progress
  • Rocket based combined cycle

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