固体超燃冲压发动机燃烧组织技术研究进展

  • 李潮隆 ,
  • 夏智勋 ,
  • 包磊 ,
  • 高显忠 ,
  • 张国斌 ,
  • 马立坤 ,
  • 罗振兵 ,
  • 邵帅 ,
  • 何湘粤
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  • 1. 国防科技大学试验训练基地
    2. 国防科技大学
    3. 国防科技大学空天科学学院

收稿日期: 2025-01-02

  修回日期: 2025-05-09

  网络出版日期: 2025-05-13

基金资助

蒸汽重整技术在高马赫数固体超燃冲压发动机中的应用研究

Research progress on combustion organization technology of scramjet fueled by solid propellant

  • LI Chao-Long ,
  • XIA Zhi-Xun ,
  • BAO Lei ,
  • GAO Xian-Zhong ,
  • ZHANG Guo-Bin ,
  • MA Li-Kun ,
  • LUO Zhen-Bing ,
  • SHAO Shuai ,
  • HE Xiang-Yue
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Received date: 2025-01-02

  Revised date: 2025-05-09

  Online published: 2025-05-13

摘要

固体超燃冲压发动机具有结构简单、存贮便捷、发射速度快、比推力大等突出优势,有望成为未来高超声速导弹的优选动力,具有重要的军事应用价值。本文基于目前使用固体燃料的超燃冲压发动机燃烧组织技术研究现状,针对固体燃料超燃冲压发动机、固体火箭超燃冲压发动机和固体粉末超燃冲压发动机这三类典型固体超燃冲压发动机进行了综述。首先,介绍了三类典型固体超燃冲压发动机的工作原理。其次,从发动机燃烧组织技术角度对三类固体超燃冲压发动机的研究进展进行了梳理分析。最后,从工程应用前景和未来发展方向两个方面对三类固体超燃冲压发动机进行了总结与展望。

本文引用格式

李潮隆 , 夏智勋 , 包磊 , 高显忠 , 张国斌 , 马立坤 , 罗振兵 , 邵帅 , 何湘粤 . 固体超燃冲压发动机燃烧组织技术研究进展[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2025.31752

Abstract

Scramjet fueled by solid propellant has the advantages of simple structure, convenient storage, fast launch speed and large specific thrust, which is expected to become the preferred power of hypersonic missiles in the future, and has important military application perspective. In this paper, the current research progress of combustion organization tech-nology of solid fuel scramjet, solid rocket scramjet and solid powder scramjet are reviewed. Firstly, the working principle of the three typical solid scramjet is introduced. Secondly, the research progress of three types of solid scramjet is ana-lyzed from the perspective of combustion organization technology. Finally, the three types of solid scramjet are summa-rized and prospected from two aspects of engineering application prospect and future development direction.
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