Home › Library › Glossary › Spacecraft Systems › Magnetorquer
🛰️ Spacecraft Systems

Magnetorquer

Also known as: Magnetic Torquer, Torque Rod, Magnetorquer Bar

Quick answer

A magnetorquer is an electromagnetic coil that torques a satellite by pushing against Earth's magnetic field — no fuel, no moving parts. Too gentle for precise pointing alone, it is the standard tool for dumping reaction-wheel momentum and the default attitude actuator on CubeSats.

📘 Full definition✓ Reviewed 2026-09-07
A magnetorquer is an attitude control actuator consisting of a wire coil — often wound around a ferromagnetic core, or etched into a circuit board on small satellites — that creates a magnetic dipole when energised. That dipole interacts with Earth's magnetic field to produce torque on the spacecraft, exactly as a compass needle feels a twist. The virtues are robustness itself: no propellant, no moving parts, no plume, indefinite operation on modest electrical power. The physics imposes the limit: torque can only be generated perpendicular to the local field line, so full three-axis authority is impossible at any instant — control schemes exploit the field's changing direction around each orbit to reach all axes over time. In practice magnetorquers fill two roles: on larger satellites they quietly unload the momentum that accumulates in reaction wheels, replacing thruster firings and saving propellant; on CubeSats and small satellites they often *are* the attitude system, providing detumbling after deployment and coarse pointing at a few degrees. Beyond roughly 1,000 km their leverage fades with the field strength, making them a distinctly low-orbit technology.
Principle
Magnetic dipole × Earth B-field
Moving Parts
None
Precision
Low (1–5°)
Key Use
Momentum dumping for reaction wheels

Understanding Magnetorquer

Torque rods, air coils and printed coils

Three constructions dominate. Torque rods wrap thousands of turns around a permeable core that multiplies the dipole per watt — compact and strong, with slight residual magnetism as the cost. Air-core coils trade bulk for perfect linearity. CubeSats embed flat spiral coils directly in solar-panel PCBs — zero added parts, dipole for free. Sizing balances dipole strength against mass and the magnetic cleanliness the payload demands: a strong rod next to a sensitive magnetometer is its own interference problem.

The wheel's quiet partner

On most LEO satellites the operational marriage is wheels-plus-torquers: wheels do the precise, fast pointing; torquers run a slow outer loop that keeps average wheel speeds centred, dumping the momentum that gravity-gradient and aerodynamic torques pump in each orbit. The pairing removes the classic propellant tax on momentum management — one reason electric-era satellites can fly missions with almost no chemical propellant at all.

See it live Thousands of CubeSats holding attitude on magnetorquers are crossing the sky now. Open Live Globe →
📖 Learn More

Frequently Asked Questions

Tiny — micro- to millinewton-metres, thousands of times weaker than wheels or thrusters. Effectiveness comes from persistence: applied continuously over orbits, gentle magnetic torque detumbles a spinning satellite in days and steadily bleeds momentum from wheels.
The torque law: torque = dipole × field, always perpendicular to the local magnetic field vector. The axis parallel to the field is momentarily uncontrollable. Because the field direction rotates as the satellite orbits, that blind axis keeps moving — controllers schedule around it, achieving three-axis authority on average rather than instantaneously.
The beautifully simple algorithm every CubeSat flies: command each coil's dipole proportional to the negative rate of change of the measured field (−dB/dt). No attitude knowledge needed — just a magnetometer — and the physics guarantees rotational energy drains until the tumble stops.

Sources & References

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