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固体超燃冲压发动机燃烧组织技术研究进展

李潮隆 何湘粤 夏智勋 包磊 高显忠 郭正涛 张国斌 马立坤 罗振兵 邵帅

航空学报2025,Vol.46Issue(18):1-19,19.
航空学报2025,Vol.46Issue(18):1-19,19.DOI:10.7527/S1000-6893.2025.31752

固体超燃冲压发动机燃烧组织技术研究进展

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

李潮隆 1何湘粤 1夏智勋 2包磊 1高显忠 1郭正涛 1张国斌 1马立坤 2罗振兵 2邵帅1

作者信息

  • 1. 国防科技大学 试验训练基地,西安 710000
  • 2. 国防科技大学 空天科学学院,长沙 410073
  • 折叠

摘要

Abstract

Scramjet fueled by solid propellant has the advantages of simple structure,convenient storage,fast launch speed and large specific thrust,making them the preferred future hypersonic missiles power with important military ap-plication value.In this paper,the current research progress of combustion organization technology for solid fuel scram-jet,solid rocket scramjet and solid powder scramjet are reviewed.Firstly,the working principle of three types of typical solid scramjet is introduced.Secondly,the research progress of three types of solid scramjet is analyzed from the per-spective of combustion organization technology.Finally,the three types of solid scramjet are summarized and pros-pected from aspects of engineering application prospect and future development direction.

关键词

固体燃料超燃冲压发动机/固体火箭超燃冲压发动机/固体粉末超燃冲压发动机/燃烧组织技术/气固两相流

Key words

solid fuel scramjet/solid rocket scramjet/solid powder scramjet/combustion organization technology/gas-solid two-phase flow

分类

航空航天

引用本文复制引用

李潮隆,何湘粤,夏智勋,包磊,高显忠,郭正涛,张国斌,马立坤,罗振兵,邵帅..固体超燃冲压发动机燃烧组织技术研究进展[J].航空学报,2025,46(18):1-19,19.

基金项目

国防科技大学青年自主创新科学基金(ZK24-62,ZK24-63) (ZK24-62,ZK24-63)

国家自然科学基金(12502325) National University of Defense Technology Youth Independent Innovation Scientific Fund(ZK24-62,ZK24-63) (12502325)

National Natural Science Foundation of China(12502350) (12502350)

航空学报

OA北大核心

1000-6893

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