Thrusters (spacecraft)

Thruster is a propulsive device used by spacecraft for station keeping, altitude 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.^{[1][2][3][4][5]}

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

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

See also[]

• Liquid Apogee Engine – A liquid-propellant rocket used as the primary propulsion device on geostationary orbit satellites.
• Apogee kick motor – A solid-fuel rocket used as the primary propulsion device to circularize satellites inserted into a transfer orbit.

References[]

Look up thruster or thrusters in Wiktionary, the free dictionary.