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Electric Propulsion

Also known as: EP, Electric Thruster, Solar Electric Propulsion, SEP

📘 Definition
Electric propulsion generates thrust by using electrical energy (typically from solar panels) to ionise and accelerate a propellant. The three main EP technologies are: gridded ion thrusters (electrostatic acceleration through charged grids), Hall-effect thrusters (magnetic/electric field acceleration in an annular channel), and pulsed plasma thrusters (electromagnetic acceleration of plasma). All share the same trade-off: extremely high specific impulse (fuel efficiency) but very low thrust. EP is now the standard for station-keeping on GEO communications satellites, orbit maintenance on Starlink's constellation, and primary propulsion for deep-space missions like NASA's Dawn and ESA's BepiColombo.
1,500–5,000 s
Specific Impulse
mN to 1 N
Thrust
Solar panels (or nuclear)
Power Source
Hall-effect (krypton)
Starlink Thruster

Understanding Electric Propulsion

Types of Electric Propulsion

TypeHow It WorksIsp (s)Example Use
Gridded IonIons accelerated through electrostatic grids2,000–5,000NASA Dawn, DART
Hall-EffectIons accelerated by crossed electric/magnetic fields1,500–3,000Starlink, Eutelsat GEO sats
Pulsed PlasmaElectromagnetic pulses ablate solid propellant600–2,000CubeSats
ElectrosprayElectric field extracts and accelerates ions from liquid500–5,000Accion TILE thrusters

Why Electric Propulsion Is Growing

As launch costs have fallen, the economics of satellite operations have shifted. EP allows satellites to be launched into lower, cheaper orbits and then slowly spiral up to their operational altitude under their own power — saving on launch costs at the expense of weeks or months of transit time. This approach, called electric orbit raising, is now standard for large GEO communications satellites and is used by every Starlink satellite for orbit raising, station-keeping, and end-of-life deorbit.

Deep Space Applications

Electric propulsion shines on long-duration deep-space missions. NASA's Dawn spacecraft accumulated over 11 km/s of delta-v using its three NSTAR ion thrusters — more than any spacecraft in history. ESA's BepiColombo is using ion thrusters for its 7-year journey to Mercury. Future missions to the outer solar system and asteroid belt will rely increasingly on solar or nuclear electric propulsion to achieve trajectories that chemical rockets cannot.

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Frequently Asked Questions

Yes. Every Starlink satellite carries Hall-effect thrusters fuelled by krypton gas. These are used for orbit raising after deployment (spiralling from the injection orbit to the operational altitude of 550 km), station-keeping (maintaining precise orbital positions within the constellation), collision avoidance manoeuvres, and controlled deorbit at end of life.
Electric propulsion can reach Mars and has been proposed for cargo delivery missions, where transit time is less critical. NASA's Gateway lunar station will use a large solar electric propulsion module. However, for crewed Mars missions, the multi-month transit time of EP is a concern due to radiation exposure — hybrid architectures combining chemical burns for fast departure with EP for trajectory correction are being studied.