ADCS Systems - Page 2

28 ADCS Systems from 9 Manufacturers meet your specification.
28 ADCS Systems from 9 Manufacturers
28 Products from 9 Manufacturers
Page 2 of 2
Description:Attitude Control System for CubeSats & LEO Applications

Product Specs

Satellite Type:
CubeSat
Mass:
1.230 Kg
Momentum:
50 mNms
Volume:
0.75 U
Pointing Accuracy:
0.0030 to 0.0070 Degrees
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
Description:10CM Integrated Attitude Determination and Control System

Product Specs

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
Description:Attitude Determination and Control System for SmallSats

Product Specs

Satellite Type:
SmallSat
Mass:
16 Kg
Pointing Accuracy:
0.0170 Degrees
Power Consumption:
80 W
Space Heritage:
Yes
more info
Description:Attitude Control System for CubeSats

Product Specs

Satellite Type:
CubeSat
Component:
Star Tracker, Sun Sensor, Reaction Wheel, Torquer Rod
Mass:
1.10 Kg
Torque:
5 mNm
Momentum:
15 mNms
Volume:
0.5 U
Pointing Accuracy:
0.00300 to 0.0070 Degrees
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
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Description:Integrated ADCS systems for CubeSats and SmallSats

Product Specs

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
Description:Attitude Determination and Control System for CubeSats

Product Specs

Satellite Type:
CubeSat
Mass:
2 Kg
Pointing Accuracy:
0.050 Degrees
Power Consumption:
8 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info
Description:Attitude Determination and Control System for Large CubeSats

Product Specs

Satellite Type:
CubeSat
Mass:
2 Kg
Pointing Accuracy:
0.050 Degrees
Power Consumption:
10 W
Space Heritage:
Yes
Spacecraft Lifetime:
5 yrs
more info
Description:40m Integrated ADCS for CubeSats and SmallSats

Product Specs

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
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Description:Integrated Attitude Determination and Control System

Product Specs

Satellite Type:
NanoSat, MicroSat
Component:
Magnetorquer, Gyroscope
Mass:
0.44 Kg
Torque:
13 mNm
Momentum:
13 mNms
Volume:
0.7 U
Pointing Accuracy:
0.40 Degrees
Supply Voltage:
3.3 to 5 V
Power Consumption:
2.70 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:20m Integrated ADCS for CubeSats and SmallSats

Product Specs

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
Description:Integrated ADCS for CubeSats

Product Specs

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
Description:Integrated ADCS systems with Reaction Sphere

Product Specs

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
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Description:CubeSats ranging from 6U to 16U, ADCS needs larger output torque

Product Specs

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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