Thrust Chamber Design
Thrust Chamber Design is a methodological framework within the field of rocket propulsion that specifies the systematic integration of geometric, thermodynamic, and material parameters to optimize combustion efficiency, heat transfer management, and structural integrity in the combustion chamber and nozzle assembly of liquid rocket engines.
106
Publications
2.7K
Citations
314
Authors
93
Institutions
Publications per year
2017–2026
12
106
History of liquid propellant rocket engines
Choice Reviews Online · 2006 · 123 citations
Engineering, Aerospace Engineering, Mechanical Engineering +13
1–5 of 106
314
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
4 publications · 77 citations
4
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3
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3
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1–5 of 314
93

Glenn Research Center
Cleveland, United States
11 h-index
22 publications
544 citations
Marshall Space Flight Center
Redstone Arsenal, United States
8 h-index
16 publications
607 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
7 h-index
20 publications
388 citations

Beihang University
Beijing, China
6 h-index
18 publications
390 citations
Kyushu University
Fukuoka, Japan
3 h-index
13 publications
200 citations
The University of Osaka
Osaka, Japan
3 h-index
6 publications
97 citations

Centre National de la Recherche Scientifique
Paris, France
2 h-index
4 publications
176 citations
Institute for Laser Technology
Osaka, Japan
2 h-index
2 publications
25 citations
1–8 of 93
19 publications · 374 citations
13
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8 publications · 258 citations
7
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5 publications · 172 citations
5
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AST · 3 publications · 78 citations
3
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3 publications · 137 citations
3
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