High Torque reaction wheel for 35 – 100 kg satellites.
Serving micro satellite missions with a minimum of 5 years lifetime.
Providing a Momentum capacity of 0.5 Nms and offering a Torque of 50 (up to 100) mNm, with a mass of 850 g and volume 97 x 97 x 40 mm.
Optimised for less than 3.5 W at nominal Momentum.
State-of-the-art design: Low magnetic residual, very high radiation shielding, redundant windings, firmware updates in space and regenerative braking.
Based on technology with 36 months accumulated runtime in space and counting.