HARDWARE / PRODUCTAdded 12 Jul 2026

Reaction Wheel

Space Inventor ApS
Reaction Wheel

High-performance reaction wheel for microsatellite attitude control, available in 500 and 1000 Nms configurations.

Typed specifications1 values

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Design lifetime
5 years
as published, mode unspecified · vendor page (catalogue a

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As published by the supplier8 lines, in the manufacturer's own wording
Msrp
€55,000
Momentum capacity
500 and 1000 Nms variants
Mission lifetime
Up to 5 years
Motor
3-phase outrunner permanent magnet synchronous motor (PMSM)
Bearings
Two hybrid ceramic high-precision bearings
Interface
Redundant CAN bus via CSP
Body material
Al-6061-T6
Rotor material
Ferritic stainless steel with Neodymium magnets

About

Space Inventor’s high-performance reaction wheel units are meticulously designed for microsatellite missions with mission lifetimes of up to 5 years. These units feature an integrated 3-phase outrunner permanent magnet synchronous motor (PMSM) with fully integrated motor control electronics and software for seamless, efficient satellite attitude control.

The rotor is precisely suspended between two hybrid ceramic high-precision bearings, ensuring longevity and low friction in vacuum conditions. Each wheel operates autonomously with an internal microcontroller, controlling momentum and torque based on onboard computer commands, and includes a redundant CAN bus interface via CSP plus basic telemetry sensors (temperature, current, speed).

For comprehensive three-axis control, Space Inventor recommends a reaction wheel assembly with four wheels in a classic configuration. The 500 and 1000 Nms reaction wheels prioritize reliability through redundant stator windings and driver electronics. Construction uses Al-6061-T6 for the body, ferritic stainless steel for the rotor, and Neodymium magnets for enhanced magnetic properties.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: space-inventor.com ↗

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