ADCS Systems

13 ADCS Systems from 3 Manufacturers meet your specification.
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  • Manufacturers: Blue Canyon Technologies, AAC Clyde Space, CubeSpace Satellite Systems
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
SKU:XACT-15
Satellite Type:
CubeSat
Mass:
1.1 Kg
Torque:
5 mNm
Momentum:
15 mNms
Volume:
0.5 U
Pointing Accuracy:
±0.003 deg (1-sigma) for 2 axes ±0.007 deg (1-sigma) for 3rd axis
Supply Voltage:
12 V
Radiation Tolerance:
40 Krad
Slew Rate:
Up to 10 Deg/sec (4 kg 3U Cubesat)
Data Interface:
RS-422
Spacecraft Lifetime:
5 Years
more info
SKU:CubeADCS Y-Momentum
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
0.3 Kg
Space Heritage:
Yes
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:CubeADCS 3-Axis Small
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
0.5 Kg
Space Heritage:
Yes
more info
SKU:CubeADCS 3-Axis Medium
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
0.8 Kg
Space Heritage:
Yes
more info
Description:High-performance design compatible with a wide range of satellite configurations
Mass:
Configuration Dependent
Momentum:
B/w 500 and 8000 mNms depending on which wheels are used
Pointing Accuracy:
±0.002 deg (1-sigma), 3 axes
Supply Voltage:
5, 28 V
Slew Rate:
Application Dependent
Data Interface:
RS-422
Spacecraft Lifetime:
5 Years
more info
SKU:CubeADCS 3-Axis Large
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
1.3 Kg
Space Heritage:
Yes
more info
SKU:XACT-50
Satellite Type:
CubeSat
Mass:
1.23 kg
Momentum:
50 mNms
Volume:
0.75 U
Pointing Accuracy:
±0.003 deg (1-sigma) for 2 axes ±0.007 deg (1-sigma) for 3rd axis
Supply Voltage:
12 V
Slew Rate:
Up to 10 Deg/sec (14 kg 6U Cubesat)
Data Interface:
RS-422
Spacecraft Lifetime:
5 Years
more info
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Star Tracker, Sun Sensor, Earth Sensor
Radiation Tolerance:
24 kRad
more info

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