Spacecraft electric propulsion

Spacecraft electric propulsion encompasses spacecraft propulsion systems that use electric energy to accelerate and expel propellant, generating thrust through electric or magnetic fields. Their principal advantage over chemical rockets is much higher specific impulse, meaning greater propellant efficiency, but the limited electrical power available aboard spacecraft yields much lower thrust, making electric propulsion unsuitable for launch from Earth's surface and better suited to long-duration in-space maneuvers.

Source: Wikipedia — Spacecraft electric propulsion (CC BY-SA 4.0)