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The thrust performance of the converging rotating detonation engine (converging RDE) was 94 to 100% of the theoretical rocket thrust performance. This study shows that detonation combustion can significantly reduce engine weight while maintaining thrust performance.
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This page is a summary of: Thrust Performance of Converging Rotating Detonation Engine Compared with Steady Rocket Engine, Journal of Propulsion and Power, February 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38784.
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