ADCS Systems from Manufacturers in Czech Republic

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Description:Attitude Determination and Control System (ADCS) for CubeSats

Product Specs

Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Magnetometer, Gyroscope
Mass:
0.4243 Kg
Torque:
0.20 mNm
Momentum:
0.60 mNms
Pointing Accuracy:
1 Degree
Supply Voltage:
5 to 8 V
Power Consumption:
0.375 to 1.4 W
Radiation Tolerance:
36 krad
Data Interface:
CAN, I2C, UART
Spacecraft Lifetime:
3 yrs
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Data Interface