Reaction Wheels

113 Reaction Wheels for Space Applications from 31 manufacturers listed on SatNow

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.

Description:CubeSats Low Mass, Low Power Reaction Control Wheels
Satellite Type:
CubeSat, NanoSat, PicoSat
Torque:
2 mNm
Angular Momentum:
3 to 6 mNms
Supply Voltage:
3.25 to 3.5 V
Operating Temperature:
-20 to 60 Degree C
Interface:
I2C
more info
Description:Reaction Wheel for SmallSats
Satellite Type:
SmallSat
Torque:
0.005 nNm
Angular Momentum:
0.1 Nms
Mass:
0.5 Kg
Speed:
5000 rpm
Operating Temperature:
-20 to 50 Degree C
more info
Description:Reaction Wheel for Small Satellites
Satellite Type:
SmallSat
Torque:
14.2 to 16 mNm
Angular Momentum:
0.5 Nms
Mass:
1.55 (RW + WDE), 1.70 (RW + WDE + Gyro) Kg
Speed:
500 to 5000 rpm
Supply Voltage:
5 (Electronics), 17 to 32 V (Motor)
Power Consumption:
0.5 W
Space Heritage:
Yes
Storage Temperature:
-30 to 50 Degree C
Operating Temperature:
-20 to 40 Degree C
Interface:
UART, RS-422
more info
Description:43 W Low Cost Light Weight Reaction Wheel
Torque:
0.05 Nm
Angular Momentum:
2 Nms
Mass:
32 Kg
Supply Voltage:
22 to 34 V
Power Consumption:
43 W
Interface:
CAN
more info
Description:Reaction Wheel System for CubeSat
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
Description:High Torque Reaction Wheel for Satellites
Torque:
248 mNm
Angular Momentum:
45 Nms
Mass:
7.45 Kg
Speed:
4000 rpm
Vibration:
IP: 10 g RMS, OoP: 15 g RMS (RWA), IP: 11.2 g RMS, OoP: 17.4 g RMS (WDE)
Static Imbalance:
0.5 g-cm
Dynamic Imbalance:
5 g-cm2
Supply Voltage:
28 to 50 V
Power Consumption:
7.6 W (Quiescent Power), 29 W (Steady State Power), 168 W (Peak Power)
Space Heritage:
Yes
Operating Temperature:
-15 to 60 Degree C (RWA), -30 to 60 Degree (WDE)
more info
Description:1 Nms Angular Momentum Reaction Wheels with advanced lubrication system for long life and vibration isolation
Torque:
70 mNm
Angular Momentum:
1 Nms
Mass:
0.95 Kg
Supply Voltage:
22 to 34 V
Power Consumption:
10 W
Space Heritage:
Yes
Interface:
RS-422
more info
Description:7 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
7 mNm
Angular Momentum:
16.2 mNms
Mass:
144 g
Speed:
10000 rpm
Vibration:
14.16 g RMS
Dynamic Imbalance:
0.014 g.cm²
Supply Voltage:
6.4 to 16.8 V (Motor Supply Voltage)
Power Consumption:
336 to 770 mW(Average Power)
Space Heritage:
Yes
Operating Temperature:
-20 to 80 Degree C(Thermal vacuum)
Interface:
CAN, UART, RS-485
more info
Description:12.0 Nms RWA RW4 Rad-Hard Reaction Wheel
Satellite Type:
SmallSat, NanoSat, MicroSat
Torque:
0.2 Nm
Angular Momentum:
12 Nms
Mass:
5 Kg
Vibration:
16.7 to 20 g RMS
Static Imbalance:
26.7 g-mm
Dynamic Imbalance:
800 g.mm²
Supply Voltage:
24 to 34 V
Power Consumption:
38 to 170 W
Space Heritage:
Yes
Storage Temperature:
-40 to 70 Degree C
Operating Temperature:
-20 to 60 Degree C
Interface:
RS-485
more info
Description:1.6 Nms Angular Momentum Reaction Wheels for Satellite Constellations
Angular Momentum:
1.6 Nms
Mass:
1.8 Kg
Space Heritage:
Yes
Interface:
RS-422, RS-485, CAN
more info

What are Reaction Wheels?

Reaction wheels or momentum wheels are flywheels that are used to provide attitude (orientation) control and stability to a spacecraft. There is no air resistance in space and as a result when a reaction wheel turns in one direction the spacecraft tends to turn in the opposite direction as per Newton’s Third Law. Therefore, by maintaining the rotation of one reaction wheel, a single axis of the spacecraft is stabilized and with a minimum of three wheels that are spinning in three directions.

The reaction wheels are fixed in place they spin at a very high rate of revolution which is around 1000-4000 revolutions per minute, which builds up angular momentum. Therefore, to change the orientation of the spacecraft the rate at which the wheel spin can be changed. As a result, this rate of change produces a torque that causes the spacecraft/satellite to change its direction. The main advantage of the technology of reaction wheels is that it works on electricity alone which means that there is no need for the use of liquid propellant to change the direction of the spacecraft.


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