Overview of Research Progress on Solid Rocket Ramjet Engines

Solid rocket ramjet engines are the ideal propulsion devices for high-speed aircraft. This article reviews the research history of solid rocket ramjet engines, analyzes the latest developments both domestically and internationally, and summarizes the key technologies that still need to be addressed in this field. These include wide-range flight inlet design, aircraft/engine integration overall technology, gas flow regulation technology, combustion organization technology, and so forth. Furthermore, it provides a summary and outlook on the future prospects of solid rocket ramjet engines, offering valuable insights for the development of related technologies in the future.

Authors

Publication Details

Journal
Springer Link (Chiba Institute of Technology)
Published
2026-04-13
DOI
https://doi.org/10.1051/epjconf/202636104001/pdf
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
0.00
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article

Overview of Research Progress on Solid Rocket Ramjet Engines

Jinchuan Hu, Yan Dong
Springer Link (Chiba Institute of Technology)
Rocket and propulsion systems research
article

Overview of Research Progress on Solid Rocket Ramjet Engines

Jinchuan Hu, Yan Dong
article en

Abstract

Solid rocket ramjet engines are the ideal propulsion devices for high-speed aircraft. This article reviews the research history of solid rocket ramjet engines, analyzes the latest developments both domestically and internationally, and summarizes the key technologies that still need to be addressed in this field. These include wide-range flight inlet design, aircraft/engine integration overall technology, gas flow regulation technology, combustion organization technology, and so forth. Furthermore, it provides a summary and outlook on the future prospects of solid rocket ramjet engines, offering valuable insights for the development of related technologies in the future.

Springer Link (Chiba Institute of Technology)
Affordable and clean energy
Openalex Percentile: Top 4%
Rocket and propulsion systems research
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