Thrust Vector Control
Thrust Vector Control is a propulsion system mechanism that actively directs the thrust output of a rocket or aircraft engine by altering the direction of the exhaust jet, thereby enabling controlled changes in vehicle trajectory and attitude.
291
Publications
9.7K
Citations
646
Authors
242
Institutions
Publications per year
2017–2026
81
291
<i>Rocket Propulsion Elements</i>
George P. Sutton, Howard S. Seifert · Physics Today · 1950 · 1.8K citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
1–5 of 291
646
8
h-index
7
h-index
6
h-index
6
h-index
5
h-index
1–5 of 646
242

Langley Research Center
Hampton, United States
14 h-index
27 publications
1.2K citations
Gyeongguk National University
Andong, South Korea
12 h-index
25 publications
769 citations
Technion – Israel Institute of Technology
Haifa, Israel
8 h-index
16 publications
373 citations
Politecnico di Milano
Milan, Italy
7 h-index
16 publications
574 citations

Shanghai Jiao Tong University
Shanghai, China
7 h-index
25 publications
545 citations
California Institute of Technology
Pasadena, United States
6 h-index
11 publications
2.1K citations
Pratt & Whitney (United States)
East Hartford, United States
5 h-index
8 publications
207 citations

Whitney Museum of American Art
New York, United States
5 h-index
8 publications
207 citations
1–8 of 242
21 publications · 733 citations
16
h-index
17 publications · 510 citations
15
h-index
14 publications · 488 citations
13
h-index
11 publications · 343 citations
11
h-index
10 publications · 229 citations
10
h-index
1–5