High Torque reaction wheel for 12-16U satellites.
Serving nano satellite missions with a minimum of 5 years lifetime.
Providing a Momentum capacity of 42 mNms and offering a Torque of 5 mNm, with a mass of 155 g and 50 x 50 x 21 mm volume.
Optimised for less than 350 mW at nominal Momentum.
The rotor is axially suspended between two hybrid ceramic high precision bearings chosen for long life and low friction in extreme conditions.
Based on technology with 36 months accumulated runtime in space and counting.