CubeSat ADCS Systems

18 CubeSat ADCS Systems from 8 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
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: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: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
Description:Fully Integrated, Adaptable, Plug and Play Attitude Determination and Control System
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Magnetometer, Gyroscope
Mass:
0.4243 g
Torque:
0.2 mNm
Momentum:
0.6 mNms
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
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
Description:1.5 Degree, Attitude Determination & Control System for Micro Satellite
Satellite Type:
CubeSat, MicroSat
Mass:
8 Kg
Pointing Accuracy:
1.5 Degree
Power Consumption:
35 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
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
Description:0.05 Degree, Attitude Determination & Control System for Micro Satellite
Satellite Type:
CubeSat, MicroSat
Mass:
10 Kg
Pointing Accuracy:
0.05 Degree
Power Consumption:
38 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info

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Space Heritage

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