Liquid Rocket Engines
Liquid Rocket Engines is a chemical rocket propulsion system that generates thrust by burning liquid propellants—stored in separate tanks and delivered under pressure to a combustion chamber—so that the high-temperature, high-velocity exhaust gases produced are expanded and expelled through a nozzle.
484
Publications
16.1K
Citations
1.1K
Authors
279
Institutions
Publications per year
2017–2026
119
Variants
Liquid-propellant Rocket Engines
Parents
484
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Korea Aerospace Research Institute
Daejeon, South Korea
16 h-index
48 publications
1.2K citations
Marshall Space Flight Center
Redstone Arsenal, United States
15 h-index
43 publications
1.3K citations

Sapienza University of Rome
Rome, Italy
14 h-index
51 publications
1.3K citations

Beihang University
Beijing, China
13 h-index
37 publications
1.1K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
13 h-index
48 publications
3K citations

Glenn Research Center
Cleveland, United States
13 h-index
24 publications
692 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
12 h-index
42 publications
727 citations

Northwestern Polytechnical University
Xi'an, China
12 h-index
37 publications
900 citations
1–8 of 279
62 publications · 3.3K citations
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25 publications · 1K citations
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Repository · 15 publications · 889 citations
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AST · 12 publications · 386 citations
12
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8 publications · 150 citations
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