HARDWARE / PRODUCTUpdated 25 Jul 2026

Reaction Wheel RWT250

EXA (Astro-und Feinwerktechnik)
Reaction Wheel RWT250

The RWT250 is a reaction wheel designed for small satellites, featuring integrated wheel drive electronics, various operation modes, and extensive housekeeping data.

Typed specifications19 values

Discloses 5 of 10 fields engineers filter by in this category (category median 5).

Mass
3 000 g
as published, mode unspecified · vendor page (catalogue a 3 000 g max
Envelope (L×W×H)
200mm*200mm*100mm
datasheet p.1
Angular momentum storage
4 N·m·s
@5000rpm · datasheet p.1 4 N·m·s 5000rpm
Max torque
300 mN·m
nom. · datasheet p.1 300 mN·m as published, mode unspecified
Speed range
5 000 rpm
nom. · datasheet p.1 5 000 rpm max  |  5 000 rpm max · maximum rotation speed
Supply voltage
23–34 V
as published, mode unspecified · vendor page (catalogue a
Power consumption
3 W
as published, mode unspecified · vendor page (catalogue a
Operating temperature
-20–50 °C
operational · datasheet p.1
Design lifetime
7 years
datasheet p.1
Survival temperature
-30 °C
product page
Satellite class
microsat 10-100 kg
SmallSat TorqueLine · datasheet p.0
Continuous (nominal) torque
300 mN·m
printed 0.3 Nm · datasheet p.1
Nominal operating speed
5 000 rpm
datasheet p.1
Flywheel moment of inertia
0.008 kg·m²
datasheet p.1

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 supplier16 lines, in the manufacturer's own wording
Angular momentum
4.0 Nms @ nominal speed
Nominal rotation speed
5000 rpm
Nomial reaction torque
0.3 Nm Max. commandable deliverable output torque over the whole speed range
Supply voltage
23 to 34 V
Power consumption
≤ 3.0 W Stand by (motor off)
Power consumption (2)
≤ 15.0 W @ 5000 rpm
Power consumption (max)
≤ 200 W Maximum (max. torque/max. speed)
Mass
≤ 3.0 kg
Moment of inertia
7.64e-3 kg m2 Rotating mass
Dimensions
Height: ≈100 mm Diameter: 200 mm
Operation temperature
-20 °C to +50 °C
Start-up temperature
-30 °C to +60 °C
Survival temperature
-30 °C to +70 °C
Data interface
RS485/CAN
Design lifetime
> 7 years (Depending on electronics grade (up to 10 years))
Storage time
> 3 years (incl. 240 h of ground operation)

About

The RWT250 is a reaction wheel specifically developed for small satellites, providing precise attitude control. It incorporates integrated wheel drive electronics with latch-up protection, ensuring robust operation. The device offers different operation modes for speed and acceleration, managed by model-based controllers, which contribute to high torque and speed stability with low noise. It provides extensive housekeeping data, including speed, voltage, current, and temperatures, for monitoring and diagnostics. The RWT250 features internal compensation for friction and time delays, and its mechanical design, high level of alignments, and balancing result in low emitted vibrations. It is designed for a lifetime of over 7 years, potentially up to 10 years depending on the electronics grade, and has a storage time of over 3 years (including 240 hours of ground operation).

Documentation

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

Source: www.astrofein.com ↗

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