ADCS Systems - Page 2

34 ADCS Systems from 9 Manufacturers meet your specification.
SKU:CubeADCS 3-Axis Small
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
0.5 Kg
Space Heritage:
Yes
more info
SKU:READY-200HP
Satellite Type:
SmallSat
Mass:
19 Kg
Pointing Accuracy:
0.006 Degree
Power Consumption:
87 W
Space Heritage:
Yes
more info
SKU:CubeADCS 3-Axis Medium
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
0.8 Kg
Space Heritage:
Yes
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:CubeADCS 3-Axis Large
Satellite Type:
NanoSat
Component:
Magnetometer, Coarse Sun Sensors, Fine Sun & Earth Sensors, Star Tracker
Mass:
1.3 Kg
Space Heritage:
Yes
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
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

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Space Heritage

Data Interface