reaction flywheel

 The reaction flywheel is an important actuator for satellite attitude control, and its main components are
Including digital control circuit, drive motor, connecting cables, etc. Zero Gravity Laboratory Autonomous
The reaction flywheel system developed has the characteristics of large output torque and high control accuracy.
As an actuator for attitude control of 5KG to 50KG satellites.

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SKU: SATPLT053U-3-1-1 Category: Tag:

It has CAN communication default configuration function: the communication baud rate is configured as 500kbps;

It has parameter input protection function;

It has speed, current and torque command control functions;

It has telemetry function: it dynamically displays the control target value, actual flywheel speed, and actual motor current in the form of a label box, and the data format is float;

It has the function of real-time recording and graphic display of flywheel speed and motor current;

With data storage function: data is stored in CSV file format.


Size

Less than 45×45×21mm

Maximum angular momentum

≥8mNms

Speed range

Rated speed -6000 to 6000rpm

Speed control accuracy

Better than ± 8rpm ± 60-6000rpm

Working voltage

12V

Steady state power consumption

≤ 0.9W@6000rpm (+12V power supply, single axis)

Peak power consumption

(+12V power supply, single axis)

Communication control interface

CAN

Mass

Single wheel body 80g ± 5g

Working temperature

-15℃~+50℃

Design life

≥3years

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