ADCS Systems

16 ADCS Systems from 3 Manufacturers meet your specification.
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  • Manufacturers: Blue Canyon Technologies, Berlin Space Technologies, Tensor Tech
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: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: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
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: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: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
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: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
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

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