Detonation-based Propulsion
Detonation-Based Propulsion is a propulsion system concept that utilizes detonative combustion—characterized by supersonic exothermic reaction waves driven by shock compression—as its energy release mechanism, distinguishing it from deflagration-based systems that rely on subsonic flame propagation.
70
Publications
5.2K
Citations
182
Authors
72
Institutions
Publications per year
2017–2026
23
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1–5 of 70
182
Office National d'Études et de Recherches Aérospatiales, France
4 publications · 104 citations
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4
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3
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3
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1–5 of 182
72

United States Naval Research Laboratory
Washington, United States
6 h-index
10 publications
1.4K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
4 h-index
4 publications
199 citations
Semenov Institute of Chemical Physics
Moscow, Russia
4 h-index
6 publications
1K citations

University of Central Florida
Orlando, United States
3 h-index
9 publications
657 citations
Russian Academy of Sciences
Moscow, Russia
3 h-index
3 publications
60 citations
Innovative Scientific Solutions (United States)
Dayton, United States
3 h-index
6 publications
352 citations

Glenn Research Center
Cleveland, United States
3 h-index
5 publications
157 citations
California Institute of Technology
Pasadena, United States
3 h-index
6 publications
150 citations
1–8 of 72
12 publications · 1.2K citations
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5 publications · 960 citations
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4 publications · 227 citations
3
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2 publications · 86 citations
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2 publications · 48 citations
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