Next Article in Journal
Space Trajectory Planning with a General Reinforcement-Learning Algorithm
Next Article in Special Issue
Numerical Investigation of a Supersonic Wind Tunnel Diffuser Optimization
Previous Article in Journal
A New Aerodynamic Domain Model (ADM) for Enhancing the Reliability of Spin Flight Vehicle Simulations
Previous Article in Special Issue
Study on the Characteristics of a Composite Power System with a Tip-Jet-Driven Rotor
 
 
Font Type:
Arial Georgia Verdana
Font Size:
Aa Aa Aa
Line Spacing:
Column Width:
Background:
Review

Progress and Development of Solid-Fuel Scramjet Technologies

1
Jiangxi Hongdu Aviation Industry Group Co., Ltd., Nanchang 330024, China
2
School of Energy and Power Engineering, Beihang University, Beijing 100191, China
3
Shen Yuan College, Beihang University, Beijing 100191, China
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(4), 351; https://doi.org/10.3390/aerospace12040351
Submission received: 16 March 2025 / Revised: 11 April 2025 / Accepted: 13 April 2025 / Published: 16 April 2025
(This article belongs to the Special Issue Innovation and Challenges in Hypersonic Propulsion)

Abstract

The solid-fuel scramjet has become a potential power device for hypersonic missiles in the future and has important military application prospects due to its advantages in gas flow regulation, flame stability, and blended combustion efficiency. This paper summarizes the research progress of three types of solid-fuel scramjet, including a large number of landmark numerical and experimental results. At the same time, the research progress of supersonic steady combustion and combustion enhancement technology, thermal protection technology, and the improvement of solid-fuel and combustion performance are reviewed. On this basis, the key technologies of the solid solid-fueled scramjet are summarized, and several internal scientific problems are summarized, such as the combustion organization strategy of the wide velocity domain solid rocket scramjet, efficient combustion chamber loading and thermal bulking technology, combustion instability, etc. Finally, some suggestions for the future development of the solid-fuel scramjet are put forward.
Keywords: hypersonic propulsion; supersonic stable combustion; flame temperature; engine’s thermal protection hypersonic propulsion; supersonic stable combustion; flame temperature; engine’s thermal protection

Share and Cite

MDPI and ACS Style

Yu, W.; Hu, Y.; Zhao, S.; Wang, R. Progress and Development of Solid-Fuel Scramjet Technologies. Aerospace 2025, 12, 351. https://doi.org/10.3390/aerospace12040351

AMA Style

Yu W, Hu Y, Zhao S, Wang R. Progress and Development of Solid-Fuel Scramjet Technologies. Aerospace. 2025; 12(4):351. https://doi.org/10.3390/aerospace12040351

Chicago/Turabian Style

Yu, Wenfeng, Yun Hu, Shenghai Zhao, and Rongqiao Wang. 2025. "Progress and Development of Solid-Fuel Scramjet Technologies" Aerospace 12, no. 4: 351. https://doi.org/10.3390/aerospace12040351

APA Style

Yu, W., Hu, Y., Zhao, S., & Wang, R. (2025). Progress and Development of Solid-Fuel Scramjet Technologies. Aerospace, 12(4), 351. https://doi.org/10.3390/aerospace12040351

Note that from the first issue of 2016, this journal uses article numbers instead of page numbers. See further details here.

Article Metrics

Back to TopTop