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30 ADCS Systems from 9 Manufacturers meet your specification.
ADCS-1EO Image
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Tensor Tech - ADCS-1EO

ADCS System from Tensor Tech
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Description:1EO Integrated Attitude Determination and Control System
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
READY-6U Image
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Elecnor Deimos - READY-6U

ADCS System from Elecnor Deimos
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Description:Attitude Determination and Control System for CubeSats
Satellite Type:
CubeSat
Mass:
2 Kg
Pointing Accuracy:
0.050 Degrees
Power Consumption:
8 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info
ADCS-1CM Image
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Tensor Tech - ADCS-1CM

ADCS System from Tensor Tech
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Description:1CM Integrated Attitude Determination and Control System
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
14 Kg
Torque:
1000 mNm
Momentum:
3200 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
58 to 60 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info
READY-16U Image
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Elecnor Deimos - READY-16U

ADCS System from Elecnor Deimos
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Description:Attitude Determination and Control System for Large CubeSats
Satellite Type:
CubeSat
Mass:
2 Kg
Pointing Accuracy:
0.050 Degrees
Power Consumption:
10 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info
CUBEADCS Gen 1 Image
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CubeSpace - CUBEADCS Gen 1

ADCS System from CubeSpace
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Description:3-Axis ADCS for Attitude Stabilization & Pitch Maneuvers for CubeSats
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
ADCS-10EO Image
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Tensor Tech - ADCS-10EO

ADCS System from Tensor Tech
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Description:10EO Integrated Attitude Determination and Control System
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
75 Kg
Torque:
10000 mNm
Momentum:
32000 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
180 to 190 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info
ADCS-10CM Image
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Tensor Tech - ADCS-10CM

ADCS System from Tensor Tech
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Description:10CM Integrated Attitude Determination and Control System
Satellite Type:
SmallSat
Component:
Gyroscope
Mass:
70 Kg
Torque:
10000 mNm
Momentum:
32000 mNms
Supply Voltage:
24 to 48 V
Power Consumption:
170 to 180 W
Slew Rate:
3 to 6 Degree/sec
Space Heritage:
Yes
Data Interface:
RS-485
more info
ADCS100 Image
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Tensor Tech - ADCS100

ADCS System from Tensor Tech
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Description:Integrated ADCS for CubeSats
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Gyroscope, Magnetometer
Mass:
0.30 Kg
Torque:
1 mNm
Momentum:
10 mNms
Volume:
0.20
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
ADCS10 Image
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Tensor Tech - ADCS10

ADCS System from Tensor Tech
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Description:Integrated ADCS systems with Reaction Sphere
Satellite Type:
CubeSat
Component:
Magnetorquer, Sun Sensor, Magnetometer
Mass:
0.140 to 0.14 Kg
Volume:
0.20
Pointing Accuracy:
10 Degree
Supply Voltage:
3.3 to 5 V
Power Consumption:
1000 mW
Data Interface:
I2C, UART
more info
ADCS400 Image
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Tensor Tech - ADCS400

ADCS System from Tensor Tech
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Description:CubeSats ranging from 6U to 16U, ADCS needs larger output torque
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Gyroscope, Magnetometer
Mass:
1.2 kg
Torque:
4 mNm
Momentum:
20 mNms
Pointing Accuracy:
+/- 0.2 deg, +/- 1 deg
Supply Voltage:
3.3 to 5 V
Power Consumption:
4000 mW
Data Interface:
I2C, UART
more info
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ADCS Systems Directory