HARDWARE / PRODUCTUpdated 24 Jul 2026

MTQ800

AAC Clyde Space
MTQ800

The MTQ800 is a magnetorquer designed for attitude control in small satellites, offering a compact and efficient solution for detumbling and attitude stabilization.

Typed specifications53 values

Discloses 6 of 8 fields engineers filter by in this category (category median 3).

Magnetic dipole moment
15 A·m²
Nominal · datasheet p.1 30 A·m² Boost mode  |  15 A·m² Design  |  30 A·m² Peak  |  30 A·m² max · peak dipole moment (boost mode)  +1
Mass
489 g
typ. · datasheet p.1 489 g
Envelope (L×W×H)
60 x 70 x 14 mm
Driver Enclosure · datasheet p.2 250 x 67 x 35 mm Torquer rods
Supply voltage
12 V
nom. · datasheet p.2 8 V min  |  12.5 V max  |  8–12.5 V
Power consumption
3 W
at nominal dipole moment, including drive electronics · datasheet p.1 1.63 W Dipole moment of 10 Am2 (Max)  |  1.44 W Dipole moment of 10 Am2 (Min)  |  1.54 W Dipole moment of 10 Am2 (Typ)  |  5.52 W Dipole moment of 20 Am2 (Max)  +17
Data interface
RS-422
datasheet p.1 RS-485
Operating temperature
-45 °C
min · datasheet p.2 45 °C max  |  -45–45 °C
Radiation tolerance (TID)
10 krad
product page
TRL
9
datasheet p.1
Magnetorquer type
rod
datasheet p.2
Axes
1
datasheet p.0
Driver electronics
integrated
includes drive electronics and mounting brackets · datasheet p.1
Flight heritage
The MTQ800 magnetorquer series has been flying on numerous missions since 2020 and is at TRL 9. It is based on the company’s experience in design and development of magnetorquers for CubeSats which have been flying since 2017.
datasheet p.1
Missions flown
1
datasheet p.0
Quasi-static load
10 g
X-axis · datasheet p.2 10 g Z-axis  |  10 g max · maximum acceleration load, X-axis (TBC)  |  10 g max · maximum acceleration load, Y-axis (TBC)  |  10 g max · maximum acceleration load, Z-axis (TBC)

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier19 lines, in the manufacturer's own wording
Configuration
3-axis (X, Y, Z)
Dipole moment (each axis)
0.2 A·m²
Max current
0.5 A
Coil resistance
~22 Ω
Interface
I2C / Analog PWM
Supply voltage
5 V
Power consumption (max)
~3 W (all axes, full torque)
Operating temperature
-40°C to +85°C
Mass
~140 g
Dimensions
~100 x 100 x 22 mm (main board)
Radiation tolerance
10 KRad
TRL level
9
Core type
Air-core or ferromagnetic (configurable)
Linearity
>99%
Hysteresis
<1%
Pwm frequency
1-10 kHz
Current accuracy
<1%
EMI shielding
Optional
Mounting
PCB-stack or panel-mount

About

The MTQ800 is a magnetorquer, a crucial component for attitude determination and control systems (ADCS) in satellites. Magnetorquers generate magnetic dipole moments that interact with the Earth’s magnetic field to produce torque, which can be used for spacecraft detumbling, attitude stabilization, and coarse pointing. This particular model is likely designed for small satellite platforms, given the manufacturer’s focus on MicroSats and CubeSats, as indicated by other products on the page. While specific features and configurations are not detailed on this product page, magnetorquers typically offer low power consumption and a compact form factor, making them suitable for missions with strict mass and volume constraints. The presence of a dedicated PDF datasheet suggests more detailed specifications are available.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: www.aac-clyde.space ↗

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