Turbopump Design
Turbopump Design is a specialized engineering methodology within rocket propulsion systems that entails the systematic development and integration of high-speed pump and turbine components to achieve efficient, reliable delivery of propellants to the combustion chamber under extreme operational conditions.
116
Publications
2.9K
Citations
316
Authors
102
Institutions
Publications per year
2017–2026
15
116
1–5 of 116
316
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h-index
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4
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1–5 of 316
102

Glenn Research Center
Cleveland, United States
11 h-index
13 publications
409 citations

Korea Aerospace Research Institute
Daejeon, South Korea
7 h-index
21 publications
419 citations
Marshall Space Flight Center
Redstone Arsenal, United States
6 h-index
12 publications
250 citations
IHI Corporation (Japan)
Tokyo, Japan
5 h-index
8 publications
130 citations

Tohoku University
Sendai, Japan
4 h-index
4 publications
66 citations

Xi'an Jiaotong University
Xi'an, China
4 h-index
16 publications
389 citations
École Polytechnique Fédérale de Lausanne
Lausanne, Switzerland
3 h-index
6 publications
174 citations
Texas A&M University
College Station, United States
3 h-index
4 publications
80 citations
1–8 of 102
9 publications · 196 citations
9
h-index
8 publications · 352 citations
8
h-index
7 publications · 89 citations
7
h-index
5 publications · 195 citations
5
h-index
AST · 4 publications · 76 citations
4
h-index
1–5