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Hall-Effect Thruster

Also known as: Hall Thruster, HET, Stationary Plasma Thruster

Quick answer

A Hall-effect thruster is an electric rocket engine that ionises a noble gas — usually xenon or krypton — and accelerates the ions electrostatically for gentle, extremely efficient thrust. It is the workhorse of modern satellite propulsion, flying on thousands of constellation satellites.

📘 Full definition✓ Reviewed 2026-09-07
A Hall-effect thruster is a form of electric propulsion that traps electrons in a circular Hall current using crossed electric and magnetic fields, then uses them to ionise a propellant gas and accelerate the resulting ions out of an annular channel. Thrust is tiny — tens to hundreds of millinewtons, roughly the weight of a few coins — but specific impulse reaches 1,500–3,000 seconds, several times better than any chemical rocket, so far less propellant does far more work. That efficiency has made Hall thrusters the default engine of the mega-constellation era: Starlink satellites use them (burning krypton and, on newer versions, argon instead of costlier xenon) for orbit raising, collision avoidance and station-keeping, and they routinely perform end-of-life deorbit burns. Their limitation is time: manoeuvres that a chemical engine completes in minutes take a Hall thruster weeks of continuous, gentle thrusting.
Specific impulse
1,500–3,000 s
vs ~450 s for the best chemical engines
Thrust class
20–600 mN
gentle but continuous for weeks
Propellant
Xenon / krypton / argon
inert noble gases
Flies on
Starlink & most LEO constellations
plus GEO comsats since the 1970s

Understanding Hall-Effect Thruster

How the Hall current works

The thruster's magic is a magnetic field strong enough to trap light electrons but far too weak to deflect heavy ions. Electrons emitted by a cathode drift into the annular discharge channel and get caught circling it — the Hall current. Propellant gas fed into the channel collides with these circling electrons and ionises. The ions, barely feeling the magnetic field, are accelerated out of the channel by the electric field at up to 20 km/s. A fraction of the cathode's electrons leaves with the beam to neutralise it, keeping the spacecraft electrically balanced.

Hall thrusters vs other propulsion

TypeSpecific impulseThrustBest for
Chemical (bipropellant)~300–450 skN classLaunch, fast transfers
Hall-effect thruster1,500–3,000 s20–600 mNOrbit raising, station-keeping
Gridded ion thruster2,500–4,000+ s20–250 mNDeep-space missions
Cold gas~60–80 smN–NSimple attitude control
See it live Watch orbit-raising in action — the Maneuver Tracker detects satellites changing their orbits, many of them under Hall-thruster power right now. Open Maneuver Tracker →
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Frequently Asked Questions

Efficiency and mass. A Hall thruster does the same orbit-raising work as a chemical engine while carrying a fraction of the propellant, which means more of each satellite's mass budget goes to payload — decisive economics when you are building thousands of satellites.
Slowly. Thrust is measured in millinewtons, so raising a Starlink satellite from its ~300 km insertion orbit to its ~550 km operational shell takes weeks of near-continuous thrusting, spiralling gradually upwards rather than performing discrete burns.
Traditionally xenon, which ionises easily and stores densely. Its cost and scarcity pushed Starlink to krypton and then argon — cheaper and more abundant, at some cost in efficiency. All are inert noble gases, so nothing actually "burns".

Sources & References

Definitions are reviewed against primary sources. Last reviewed: 2026-09-07.