Thrust Vector Actuators
Thrust Vector Actuators is a mechanical system that enables controlled deflection of rocket engine thrust by precisely translating guidance commands into angular displacements of the nozzle or thrust chamber, thereby generating controlled directional forces for vehicle attitude and trajectory control.
20
Publications
425
Citations
73
Authors
29
Institutions
Publications per year
2017–2026
7
Variants
Thrust Vector Actuator
Parents
20
1–5 of 20
73
United States Naval Research Laboratory, United States
2 publications · 25 citations
2
h-index
2
h-index
2
h-index
United States Naval Research Laboratory, United States
2 publications · 25 citations
2
h-index
2
h-index
1–5 of 73
29

Shanghai Jiao Tong University
Shanghai, China
3 h-index
8 publications
232 citations

United States Naval Research Laboratory
Washington, United States
2 h-index
9 publications
115 citations
Science Applications International Corporation (United States)
McLean, United States
2 h-index
2 publications
25 citations
Naval Research Laboratory Laboratories for Computational Physics & Fluid Dynamics
Washington, United States
2 h-index
6 publications
75 citations
Computational Physics (United States)
Springfield, United States
2 h-index
6 publications
75 citations

China Aerospace Science and Technology Corporation
Beijing, China
1 h-index
2 publications
48 citations
University of Southampton
Southampton, United Kingdom
1 h-index
1 publications
18 citations

Beihang University
Beijing, China
1 h-index
2 publications
48 citations
1–8 of 29
Conference · 2 publications · 39 citations
2
h-index
2 publications · 37 citations
2
h-index
2 publications · 57 citations
2
h-index
1 publications · 34 citations
1
h-index
1 publications · 24 citations
1
h-index
1–5