Rocket Combustion
Rocket Combustion is a high-energy exothermic chemical reaction process within the broader domain of propulsion systems, specifically distinguished by the controlled burning of fuel and oxidizer in liquid rocket engines to generate high-pressure and high-temperature gases that produce thrust through expansion in a nozzle.
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Citations
2.6K
Authors
602
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Publications per year
2017–2026
291
1.1K
<i>Rocket Propulsion Elements</i>
George P. Sutton, Howard S. Seifert · Physics Today · 1950 · 1.8K citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
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2.6K
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
21 publications · 675 citations
15
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
12 publications · 853 citations
12
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602

Pennsylvania State University
State College, United States
26 h-index
182 publications
7.3K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
22 h-index
126 publications
3.7K citations

Northwestern Polytechnical University
Xi'an, China
19 h-index
95 publications
2.9K citations
Purdue University West Lafayette
West Lafayette, United States
18 h-index
100 publications
2.9K citations

Glenn Research Center
Cleveland, United States
18 h-index
47 publications
1.4K citations

Beihang University
Beijing, China
15 h-index
49 publications
1.4K citations
Marshall Space Flight Center
Redstone Arsenal, United States
14 h-index
36 publications
1.9K citations
Japan Aerospace Exploration Agency
Tokyo, Japan
14 h-index
47 publications
901 citations
1–8 of 602
124 publications · 6K citations
44
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48 publications · 1.8K citations
26
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51 publications · 1.7K citations
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AST · 29 publications · 1.2K citations
23
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34 publications · 1.7K citations
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