ADCS Systems - RS-485

11 ADCS Systems from 3 Manufacturers meet your specification.
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  • Data Interface: RS-485
SKU:iADCS200
Satellite Type:
CubeSat, SmallSat
Component:
Reaction Wheel, Magnetorquer, Inertial Measurement Unit
Mass:
0.4, 0.435, 0.47 kg
Torque:
0.087 mNm
Momentum:
+/- 1.5, +/- 3.0, +/- 6.0 mNms
Pointing Accuracy:
1 deg
Supply Voltage:
4 to 15 V
Power Consumption:
Idle: 1150 mW, Nominal: 1400 mW
Radiation Tolerance:
45 krad (Si)
Slew Rate:
1.52 deg/sec
Space Heritage:
Yes
Data Interface:
I2C, RS-422, RS-485, UART, CAN
more info
Description:The LEOS platform and allows full ADCS functionality including nadir pointing as well as autonomous target acquisition and tracking
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Star Tracker, Gyroscope, Magnetometer, Accelerometer
Mass:
0.4 kg
Pointing Accuracy:
1 deg
Power Consumption:
1150 mW
Space Heritage:
Yes
Data Interface:
RS-485, I2C, RS-422
more info
SKU:ADCS-10m
Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
0.44 Kg
Torque:
13 mNm
Momentum:
13 mNms
Volume:
0.7 U (Cube) or 1 Tuna-can & 0.25 U
Pointing Accuracy:
0.4 Degrees
Supply Voltage:
3.3 to 5 V
Power Consumption:
2.7 W
Radiation Tolerance:
24 krad
Slew Rate:
5 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485, UART
Spacecraft Lifetime:
3 Yrs
more info
SKU:iADCS400
Satellite Type:
CubeSat, SmallSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, GNSS Receiver, Gyroscope
Mass:
1.150, 1.300, 1.700 kg
Torque:
2 mNm
Momentum:
+/- 1.5, +/- 3.0, +/- 6.0 mNms
Pointing Accuracy:
1 deg
Supply Voltage:
4.9 to 15 V
Power Consumption:
Idle: 900 mW(2400 mW), Nominal: 2000 mW
Radiation Tolerance:
45 krad (Si)
Slew Rate:
1.57 deg/sec
Data Interface:
I2C, RS-422, RS-485, UART, CAN
more info
SKU:ADCS-20m
Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
0.75 to 0.85 Kg
Momentum:
10 to 20.8 mNms
Volume:
2 × Tuna-cans & 0.4 U to 0.5 U
Pointing Accuracy:
0.1 Degree
Supply Voltage:
3.3 to 5 V
Power Consumption:
4.4 W
Radiation Tolerance:
24 krad
Slew Rate:
5 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485, UART
Spacecraft Lifetime:
3 Yrs
more info
SKU:ADCS-MTQ
Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
0.140 Kg
Torque:
0.01 mNm
Volume:
0.2 U
Pointing Accuracy:
5 Degrees
Power Consumption:
1 W
Radiation Tolerance:
24 krad
Space Heritage:
Yes
Data Interface:
RS-485, UART
Spacecraft Lifetime:
3 Yrs
more info
SKU:ADCS-40m
Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
1.48 to 1.58 Kg
Momentum:
20 to 41.6 mNms
Volume:
4 × Tuna-cans & 0.8 U to 1 U
Pointing Accuracy:
0.1 Degree
Supply Voltage:
3.3 to 5 V
Power Consumption:
7 W
Radiation Tolerance:
24 krad
Slew Rate:
5 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485, UART
Spacecraft Lifetime:
3 Yrs
more info
SKU:ADCS-1EO
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
15 Kg
Torque:
1000 mNm
Momentum:
3200 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
62 to 64 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info
SKU:ADCS-1CM
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
14 Kg
Torque:
1000 mNm
Momentum:
3200 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
58 to 60 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info
SKU:ADCS-10EO
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
75 Kg
Torque:
10000 mNm
Momentum:
32000 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
180 to 190 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info

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