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30 ADCS Systems from 9 Manufacturers meet your specification.
ADCS-20m Image
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Tensor Tech - ADCS-20m

ADCS System from Tensor Tech
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Description:20m Integrated ADCS for CubeSats and SmallSats
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:
0.10 Degrees
Supply Voltage:
3.3 to 5 V
Power Consumption:
4.40 W
Radiation Tolerance:
24 krad
Slew Rate:
5 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485, UART
Spacecraft Lifetime:
3 Yrs
more info
FLEXCORE Image
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Blue Canyon Technologies - FLEXCORE

ADCS System from Blue Canyon Technologies
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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
ADCS-MTQ Image
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Tensor Tech - ADCS-MTQ

ADCS System from Tensor Tech
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Description:Integrated ADCS systems for CubeSats and SmallSats
Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
0.140 Kg
Torque:
0.01 mNm
Volume:
0.20
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
READY-100 Image
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Elecnor Deimos - READY-100

ADCS System from Elecnor Deimos
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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
XACT-50 Image
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Blue Canyon Technologies - XACT-50

ADCS System from Blue Canyon Technologies
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Description:Attitude Control System for CubeSats & LEO Applications
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
CubeADCS Core GEN 2 Image
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CubeSpace - CubeADCS Core GEN 2

ADCS System from CubeSpace
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Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Star Tracker, Sun Sensor, Earth Sensor
Radiation Tolerance:
24 kRad
more info
ADCS-40m Image
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Tensor Tech - ADCS-40m

ADCS System from Tensor Tech
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Description:40m Integrated ADCS for CubeSats and SmallSats
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:
0.10 Degrees
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
READY-100HP Image
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Elecnor Deimos - READY-100HP

ADCS System from Elecnor Deimos
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Description:Attitude Determination and Control System for Micro Satellites
Satellite Type:
CubeSat, MicroSat
Mass:
10 Kg
Pointing Accuracy:
0.050 Degrees
Power Consumption:
38 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info
XACT-100 Image
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Blue Canyon Technologies - XACT-100

ADCS System from Blue Canyon Technologies
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Description:Attitude Control System (ACS) for 6U CubeSats
Satellite Type:
CubeSat
Mass:
1.813 Kg
Momentum:
100 mNms
Volume:
0.5 U
Pointing Accuracy:
0.0030 to 0.0070 Degrees
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
CubeNode GEN 2 Image
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CubeSpace - CubeNode GEN 2

ADCS System from CubeSpace
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Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Star Tracker, Sun Sensor, Earth Sensor
Radiation Tolerance:
24 kRad
Data Interface:
CAN
more info
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