ADCS Systems - CAN

7 ADCS Systems from 5 Manufacturers meet your specification.
Selected Filters Reset All
  • Data Interface: CAN
SKU:iADCS200
Satellite Type:
CubeSat, SmallSat
Component:
Reaction Wheel, Magnetorquer, Inertial Measurement Unit
Mass:
0.4, 0.435, 0.47 kg
Torque:
0.087 mNm
Momentum:
+/- 1.5, +/- 3.0, +/- 6.0 mNms
Pointing Accuracy:
1 deg
Supply Voltage:
4 to 15 V
Power Consumption:
Idle: 1150 mW, Nominal: 1400 mW
Radiation Tolerance:
45 krad (Si)
Slew Rate:
1.52 deg/sec
Space Heritage:
Yes
Data Interface:
I2C, RS-422, RS-485, UART, CAN
more info
SKU:Arcus ACDS (KU Leuven ADCS)
Satellite Type:
CubeSat
Component:
Gyroscope, Photodiode, Magnetometer, Star Tracker, Reaction Wheel, Magnetorquer, PID Controller, Coarse Controller
Mass:
0.715 kg
Torque:
0.5 mNm (RW torque)
Momentum:
4 mNms ( R.W Momentum Capacity)
Pointing Accuracy:
0.11 (Fine, Fine) to 6.3 (Coa, Coa) deg
Supply Voltage:
3.3 to 5 V
Power Consumption:
940 (Detumbling) to 1400 mW (Fine/Fine)
Slew Rate:
60 deg/sec
Data Interface:
I2C, CAN
Spacecraft Lifetime:
3 Years
more info
SKU:D-Sense
Component:
Photodiode, Thermopile, Magnetometer, Gyroscope, Camera
Mass:
0.2 kg
Power Consumption:
300 mW (Standard Operative mode), 500 mW (Camera Mode)
Data Interface:
CAN
more info
Description:Fully Integrated, Adaptable, Plug and Play Attitude Determination and Control System
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, Magnetometer, Gyroscope
Mass:
0.4243 g
Torque:
0.2 mNm
Momentum:
0.6 mNms
Supply Voltage:
5 to 8 V
Power Consumption:
0.375 to 1.4 W
Radiation Tolerance:
36 krad
Data Interface:
CAN, I2C, UART
Spacecraft Lifetime:
3 yrs
more info
SKU:iADCS400
Satellite Type:
CubeSat, SmallSat
Component:
Reaction Wheel, Magnetorquer, Sun Sensor, GNSS Receiver, Gyroscope
Mass:
1.150, 1.300, 1.700 kg
Torque:
2 mNm
Momentum:
+/- 1.5, +/- 3.0, +/- 6.0 mNms
Pointing Accuracy:
1 deg
Supply Voltage:
4.9 to 15 V
Power Consumption:
Idle: 900 mW(2400 mW), Nominal: 2000 mW
Radiation Tolerance:
45 krad (Si)
Slew Rate:
1.57 deg/sec
Data Interface:
I2C, RS-422, RS-485, UART, CAN
more info
Satellite Type:
CubeSat
Component:
Reaction Wheel, Magnetorquer, Star Tracker, Sun Sensor, Earth Sensor
Radiation Tolerance:
24 kRad
Data Interface:
CAN
more info
SKU:CUBEADCS Gen 1
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

FiltersReset All

Satellite Type

Component

Mass (Kg)

Apply

Torque (mNm)

Apply

Momentum (mNms)

Apply

Pointing Accuracy (Degrees)

Apply

Supply Voltage (V)

Apply

Power Consumption (W)

Apply

Space Heritage

Data Interface