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The flywheel is essential in controlling the satellite’s flying attitude under the steady state. Its control system guarantees the reliability and lifecycle of satellites in orbit. With the adoption of an integrated design of flywheel body and control circuits, the product, minor in size and weight and supporting both speed and torque controlling modes, has already been applied to many of the in-orbit satellites of Jilin-1 series.

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Last updated: 2022-10-20



3kg ± 0.5kg
160 mm
160 mm
120 mm
maximum torque
> 50 mN m
maximum momentum storage
2 N m s
maximum angular speed
6000 rpm
angular speed
4800 rpm
idle power
< 3 W
steady state power
≤ 10W (@6000rpm)
peak power
< 70 W
5 yr
lead time
6 to 10 mo
operating temperature
-10 to 45 C


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