CubeSat Reaction Wheels

17 CubeSat Reaction Wheels from 9 Manufacturers meet your specification.

CubeSat Reaction Wheels for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

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  • Satellite Type: CubeSat
Description:Integral 4 Reaction Wheels Redundant 3-Axis Control System, Enabling Precision Pointing Of The Small Satellite
Satellite Type:
CubeSat
Torque:
3.2 mNm, 2.5 to 5.9 mNm (4RW)
Angular Momentum:
0.02 Nms, 0.0156 Nms, 0.037 Nms
Mass:
0.137 Kg, 0.665 Kg (4RW)
Speed:
6500 rpm
Supply Voltage:
5 V
Power Consumption:
0.15 W, 0.6 W (4RW)
Operating Temperature:
-40 to 85 Degree C
Interface:
SPI, UART
more info
SKU:RW400
Satellite Type:
CubeSat
Torque:
±8 to 12 mN.m (Braking)
Angular Momentum:
0.015 Nms, 0.03 Nms, 0.05 Nms
Mass:
0.197 Kg, 0.21 Kg, 0.375 Kg
Speed:
5000 rpm
Static Imbalance:
g-cm
Dynamic Imbalance:
g-cm2
Supply Voltage:
2.3 to 5.25 V
Power Consumption:
0.075 to 15 W
Space Heritage:
Yes
Operating Temperature:
-40 to 60 Degree C
Interface:
RS-485, RS-422, I2C
more info
Description:Low Mass, Low Power Reaction Control Wheel, Which Allows Cubesats And Other Small Platforms To Control Their Attitude.
Satellite Type:
CubeSat, NanoSat
Torque:
0.1 mN.m
Angular Momentum:
0.0015 Nms, 0.003 Nms, 0.006 Nms
Mass:
0.021 Kg, 0.032 Kg, 0.048 Kg
Speed:
10000 rpm, 15000 rpm
Supply Voltage:
3.25 to 3.5 V
Power Consumption:
0.8 W
Operating Temperature:
-20 to 60 Degree C
Interface:
I2C
more info
SKU:RWP100
Satellite Type:
SmallSat, CubeSat
Torque:
7 mNm
Angular Momentum:
0.10 Nms
Mass:
0.33 Kg
Supply Voltage:
10 to 14 V
Power Consumption:
0.89 W
Space Heritage:
Yes
Interface:
RS-422
more info
SKU:CubeWheel Small
Satellite Type:
CubeSat
Torque:
0.23 nNm
Angular Momentum:
1.77 Nms
Mass:
0.06 kg
Speed:
8000 rpm
Vibration:
14 g RMS
Static Imbalance:
0.003 g-cm
Dynamic Imbalance:
0.005 g-cm
Supply Voltage:
3.3 to 16 V
Power Consumption:
0.65 W
Operating Temperature:
-10 to 60 Degree C
Interface:
I2C, UART, CAN
more info
Description:Satellite Reaction Wheel With small+ size that Allows to control the attitude of your satellite
Satellite Type:
CubeSat
Torque:
2.3 mNm
Angular Momentum:
0.0036 Nms
Mass:
0.09 Kg
Speed:
6000 rpm
Vibration:
8.9 g RMS
Static Imbalance:
0.004 g-cm
Dynamic Imbalance:
0.0014 g-cm2
Supply Voltage:
3 to 16 V
Power Consumption:
0.19 W (Average Power), 2.3 W (Peak Power)
Operating Temperature:
-10 to 60 Degree C
Interface:
I2C, UART, CAN
more info
Description:Satellite Reaction Wheel With Medium size that Allows to control the attitude of your satellite
Satellite Type:
CubeSat
Torque:
1 mNm
Angular Momentum:
0.0108 Nms
Mass:
0.15 Kg
Speed:
6000 rpm
Vibration:
8.9 g RMS
Static Imbalance:
0.004 g-cm
Dynamic Imbalance:
0.0014 g-cm2
Supply Voltage:
3 to 16 V
Power Consumption:
0.19 W (Average Power), 2.3 W (Peak Power)
Operating Temperature:
-10 to 60 Degree C
Interface:
I2C, UART, CAN
more info
Description:Satellite Reaction Wheel With Large size that Allows to control the attitude of your satellite
Satellite Type:
CubeSat
Torque:
2.3 mNm
Angular Momentum:
0.03061 Nms
Mass:
0.225 Kg
Speed:
6000 rpm
Vibration:
8.9 g RMS
Static Imbalance:
0.006 g-cm
Dynamic Imbalance:
0.005 g-cm2
Supply Voltage:
3 to 16 V
Power Consumption:
0.35 W (Average Power), 10 W (Peak Power)
Operating Temperature:
-10 to 60 Degree C
Interface:
I2C, UART, CAN
more info
Description:Reaction wheels an autonomous actuators of four flywheels with drivers integrated into 3U or larger nanosatellite
Satellite Type:
NanoSat, CubeSat, SmallSat
Torque:
0.64 to 1.2 mNm
Angular Momentum:
0.0068 Nms, 0.025 Nms
Mass:
0.52 Kg
Speed:
±6000 rpm
Vibration:
12 g RMS
Supply Voltage:
5 to 14 V
Power Consumption:
2 W
Storage Temperature:
-50 to 105 Degree C
Operating Temperature:
-30 to 85 Degree C
Interface:
CAN
more info
Description:Reaction wheels block contains four reaction wheels and provides work of three-axis orientation and stabilization system
Satellite Type:
CubeSat
Mass:
0.45 Kg
Supply Voltage:
4 to 15 V
Power Consumption:
3 W
Interface:
CAN
more info

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