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

Authors

73

  1. BR
    Banahalli R. Ratna

    United States Naval Research Laboratory, United States

    2 publications · 25 citations

    2

    h-index

  2. RR
    Ravi Ramamurti

    United States Naval Research Laboratory, United States

    2 publications · 25 citations

    2

    h-index

  3. JG
    Jason Geder

    United States Naval Research Laboratory, United States

    2 publications · 25 citations

    2

    h-index

  4. WC
    William C. Sandberg

    United States Naval Research Laboratory, United States

    2 publications · 25 citations

    2

    h-index

  5. JP
    John Palmisano

    United States Naval Research Laboratory, United States

    2 publications · 25 citations

    2

    h-index

1–5 of 73

Venues

  1. AIAA Guidance, Navigation, and Control Conference and Exhibit

    Conference · 2 publications · 39 citations

    2

    h-index

  2. Journal of Propulsion and Power

    2 publications · 37 citations

    2

    h-index

  3. IEEE Robotics and Automation Letters

    2 publications · 57 citations

    2

    h-index

  4. 1

    h-index

  5. Computers & Mathematics with Applications

    1 publications · 24 citations

    1

    h-index

1–5