MicroSat Reaction Wheels

18 MicroSat Reaction Wheels from 6 Manufacturers meet your specification.

MicroSat 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.

Selected Filters Reset All
  • Satellite Type: MicroSat
Description:Reaction/Momentum Wheel (RMW) up to 0.4 Nms angular moment is an attitude control device suitable for LEO orbits
Satellite Type:
MicroSat, SmallSat
Torque:
10 mNm
Angular Momentum:
0.4 Nms
Mass:
1.1 Kg
Speed:
-4000 to 4000 rpm
Supply Voltage:
12 to 30 V
Power Consumption:
2.5 W
Storage Temperature:
-40 to 100 Degree C
Operating Temperature:
-10 to 60 Degree C
Interface:
RS-232, CAN
more info
SKU:RW5-12.0
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:
30 to 50 V
Power Consumption:
38 to 200 W
Space Heritage:
Yes
Storage Temperature:
-40 to 70 Degree C
Operating Temperature:
-20 to 60 Degree C
Interface:
CAN
more info
SKU:MicroWheel 200
Satellite Type:
SmallSat, MicroSat, MiniSat
Torque:
30 mNm
Angular Momentum:
0.18 Nms
Mass:
0.94 kg
Speed:
10000 rpm
Static Imbalance:
0.005 g-cm
Supply Voltage:
28 V
Power Consumption:
2.5 to 7 W
Space Heritage:
Yes
Storage Temperature:
-35 to 65 Degree C
Operating Temperature:
-30 to 60 Degree C
Interface:
RS-422, RS-485
more info
SKU:WHL-200-P4
Satellite Type:
MicroSat
Torque:
25 mNm
Angular Momentum:
200 mNms
Mass:
430 g
Speed:
12000 rpm
Supply Voltage:
9 to 33.6 V
Operating Temperature:
-40 to 60 Degree C
Interface:
CAN, RS-422
more info
Description:3-6U High Production Capacity, Low Disturbance Lightweight Reaction Wheel for 100Kg Class
Satellite Type:
MicroSat
Torque:
15 mNm
Angular Momentum:
0.35 Nms
Mass:
1 Kg
Supply Voltage:
18 to 34 V
Power Consumption:
15 W
Operating Temperature:
-20 to 50 Degree C
Interface:
RS-485
more info
SKU:RW4-12.0
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
SKU:MicroWheel 4000
Satellite Type:
SmallSat, MicroSat
Torque:
100 to 110 mNm
Angular Momentum:
4 Nms
Mass:
3.3 Kg
Speed:
5250 rpm
Static Imbalance:
0.02 g-cm
Dynamic Imbalance:
0.002 g-cm2
Supply Voltage:
28 V
Power Consumption:
1.5 to 9 W
Space Heritage:
Yes
Storage Temperature:
-35 to 60 Degree C
Operating Temperature:
-30 to 55 Degree C
Interface:
RS-422, RS-485
more info
SKU:WHL-500-P4
Satellite Type:
MicroSat
Torque:
50 to 100 mNm
Angular Momentum:
500 mNms
Mass:
800 g
Speed:
7200 rpm
Supply Voltage:
20 to 35 V
Power Consumption:
2 to 67 W
Operating Temperature:
-20 to 60 Degree C
Interface:
CAN, RS-422
more info
SKU:10 mNms RW-0.01
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
±1 mNm
Angular Momentum:
0.01 Nms (Nominal), 0.018 Nms (Peak)
Mass:
0.120 Kg
Vibration:
12 g RMS
Supply Voltage:
3.4 to 6 V
Power Consumption:
1.05 W
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
I2C, UART
more info
SKU:MicroWheel 1000
Satellite Type:
SmallSat, MicroSat, MiniSat
Torque:
30 mNm
Angular Momentum:
1.1 Nms
Mass:
1.44 Kg
Speed:
10000 rpm
Static Imbalance:
0.005 g-cm
Dynamic Imbalance:
0.0005 g-cm2
Supply Voltage:
28 V
Power Consumption:
2.5 to 9 W
Space Heritage:
Yes
Storage Temperature:
-35 to 65 Degree C
Operating Temperature:
-30 to 60 Degree C
Interface:
RS-422, RS-485
more info

FiltersReset All

Satellite Type

Mission

Torque (nNm)

Apply

Angular Momentum (Nms)

Apply

Mass (Kg)

Apply

Speed (rpm)

Apply

Radiation Tolerance (krad)

Apply

Supply Voltage (V)

Apply

Power Consumption (W)

Apply

Space Heritage

Interface