// PROPULSION SYSTEMS AND ENGINE TECHNOLOGY TERM
Thrust Vector Control
Thrust Vector Control is a system that changes the direction of a rocket or jet engine's exhaust to steer the vehicle. It allows for maneuvering by pushing the vehicle in a desired direction.
TECHNICAL DEFINITION
Thrust Vector Control (TVC) is an aerospace propulsion system mechanism that manipulates the direction of an engine's exhaust plume to generate a control moment, thereby enabling attitude control, steering, and maneuverability for launch vehicles, missiles, and aircraft.
BACKGROUND
Thrust vectoring, also known as thrust vector control (TVC), is the ability of an aircraft, rocket or other vehicle to manipulate the direction of the thrust from its engine(s) or motor(s) to control the attitude or angular velocity of the vehicle.
READ MORE ON WIKIPEDIASYNONYMS & ALIASES
- TVC
- Thrust Vectoring
- Nozzle Vectoring
- Exhaust Deflection
- Directional Thrust
- Vectoring Control
USAGE NOTE
TVC is crucial for flight control, especially during launch and in space where traditional aerodynamic surfaces are ineffective.
DEVELOPERS
Organizations developing technology related to Thrust Vector Control.
Develops and manufactures advanced rocket engines and launch vehicles, including the Merlin and Raptor engines, which utilize sophisticated thrust vector control for flight stability and propulsive landing capabilities.
Develops rocket engines (e.g., BE-3, BE-4) and launch systems that incorporate thrust vector control for maneuvering and flight path management of its New Shepard and upcoming New Glenn vehicles.
A major American manufacturer of rocket, hypersonic, and electric propulsion systems for space, missile defense, and strategic systems, extensively utilizing thrust vector control in its various engine designs.
Develops and produces a wide range of aerospace propulsion systems, including solid rocket motors and liquid rocket engines, where thrust vector control is critical for missile and launch vehicle guidance.
A joint venture between Airbus and Safran, developing and manufacturing rocket propulsion systems for the Ariane launch vehicles, where thrust vector control is essential for trajectory correction and control.
Engages in research and development of advanced propulsion technologies, including various forms of thrust vector control systems for future space exploration missions and launch vehicles.
Designs and manufactures the Electron launch vehicle and Rutherford engines, which feature electric pump-fed propellants and precise thrust vector control for orbital insertion and payload delivery.
Responsible for the development and operation of Japan's H-IIA, H-IIB, and H3 launch vehicles, which employ thrust vector control systems in their main engines for flight stability and trajectory management.