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CubeSat ADCS Systems

12 CubeSat ADCS Systems from 6 Manufacturers meet your specification.

CubeSat ADCS Systems for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

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  • Satellite Type: CubeSat
iADCS400 Image
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Autonomous ADCS for SmallSats & 6U CubeSats

CubeSat ADCS System from AAC Clyde Space
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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
iADCS200 Image
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Fully autonomous Integrated ADCS system for Low Power Applications

CubeSat ADCS System from AAC Clyde Space
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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
IADCS-100 Image
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Berlin Space Technologies - IADCS-100

CubeSat ADCS System from Berlin Space Technologies
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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
XACT-15 Image
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Blue Canyon Technologies - XACT-15

CubeSat ADCS System from Blue Canyon Technologies
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Description:High-performance design compatible with a wide range of satellite configurations
Satellite Type:
CubeSat
Mass:
0.885 kg
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
Slew Rate:
Up to 10 Deg/sec (4 kg 3U Cubesat)
Data Interface:
RS-422
Spacecraft Lifetime:
5 Years
more info
XACT-50 Image
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Attitude Control System for CubeSats & LEO Applications

CubeSat ADCS System from Blue Canyon Technologies
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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
XACT-100 Image
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Attitude Control System (ACS) for 6U CubeSats

CubeSat ADCS System from Blue Canyon Technologies
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SKU:XACT-100
Satellite Type:
CubeSat
Mass:
0.433 + 1.38 kg (Wheels + Torque Rods)
Momentum:
100 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
Slew Rate:
Up to 10 Deg/sec (25 kg 12U Cubesat)
Data Interface:
RS-422
Spacecraft Lifetime:
5 Years
more info
CubeADCS Y-Momentum Image
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ADCS for Nadir Pointing and Orientation Control for CubeSats

CubeSat ADCS System from CubeSpace
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SKU:CubeADCS Y-Momentum
Satellite Type:
CubeSat
Component:
Torquer Coil, Torquer Rod, Sun Sensor, Magnetometer, Reaction Wheel, Star Tracker
Mass:
0.3 kg
Supply Voltage:
3.3V, 5V, VBat (6.5V -16V)
Power Consumption:
571 to 2295 mW
Radiation Tolerance:
20 Krad
Data Interface:
I2C, UART, CAN
more info
CubeADCS 3-Axis Image
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3-Axis ADCS for Attitude Stabilization & Pitch Maneuvers for CubeSats

CubeSat ADCS System from CubeSpace
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SKU:CubeADCS 3-Axis
Satellite Type:
CubeSat
Component:
Star Tracker, Sun Sensor, Earth Sensor, Magnetometer, Reaction Wheel, Torquer Coil, Torquer Rod
Mass:
0.5 to 1.3 Kg
Supply Voltage:
3.3V, 5V, VBat(6.5V –16V)
Power Consumption:
570 to 2300 mW
Radiation Tolerance:
20 Krad
Space Heritage:
Yes
Data Interface:
I2C, UART, CAN
more info
Arcus ACDS (KU Leuven ADCS) Image
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Autonomous ADCS for Nadir, Zenith, Sun, and LLA Pointing for CubeSats

CubeSat ADCS System from CubeSat Pointing
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SKU:Arcus ACDS (KU Leuven ADCS)
Satellite Type:
CubeSat
Component:
Gyroscope, Photodiode, Magnetometer, Star Tracker, Reaction Wheel, Magnetorquer, PID Controller, Coarse Controller
Mass:
0.715 kg
Torque:
0.5 mNm (RW torque)
Momentum:
4 mNms ( R.W Momentum Capacity)
Pointing Accuracy:
0.11 (Fine, Fine) to 6.3 (Coa, Coa) deg
Supply Voltage:
3.3 to 5 V
Power Consumption:
940 (Detumbling) to 1400 mW (Fine/Fine)
Slew Rate:
60 deg/sec
Data Interface:
I2C, CAN
Spacecraft Lifetime:
3 Years
more info
ADCS100 Image
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Integrated ADCS for CubeSats

CubeSat ADCS System from Tensor Tech
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SKU:ADCS100
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Gyroscope, Magnetometer
Mass:
0.3 kg
Torque:
1 mNm
Momentum:
10 mNms
Volume:
0.2U + 64 mm dia
Pointing Accuracy:
+/- 0.2 deg, +/- 1 deg
Supply Voltage:
3.3 to 5 V
Power Consumption:
1000 mW
Space Heritage:
Yes
Data Interface:
I2C, UART
more info
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ADCS Systems Directory