Trisha Shetty (Editor)

Thrusters (spacecraft)

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit

A thruster is a propulsive device used by spacecraft for station keeping, attitude control, in the reaction control system, or long-duration, low-thrust acceleration. A vernier engine or gimbal engine is a particular case used on launch vehicles where a secondary rocket or other high thrust device is used to control the attitude of the rocket while the primary thrust engine (generally also a rocket engine) is fixed to the rocket and supplies the principal amount of thrust.

Some devices that are use or proposed to use as thrusters are:

  • Rocket engine, using exothermic chemical reactions of the propellant(s)
  • Electrohydrodynamic thruster, using ionized air (only for use in an atmosphere)
  • Electrostatic ion thruster, using high-voltage electrodes
  • Ion thruster, using beams of ions accelerated electrically
  • Hall effect thruster, a type of ion thruster
  • Pulsed inductive thruster, a pulsed form of ion thruster
  • Magnetoplasmadynamic thruster, electric propulsion using the Lorentz force
  • Electrodeless plasma thruster, electric propulsion using ponderomotive force
  • Pulsed plasma thruster, using current arced across a solid propellant
  • RF resonant cavity thruster, an electromagnetic thruster using microwaves
  • References

    Thrusters (spacecraft) Wikipedia