Reaction Wheels - Page 5

113 Reaction Wheels from 31 Manufacturers meet your specification.
Description:RS100 Reaction Sphere
Satellite Type:
CubeSat
Torque:
1 mNm
Angular Momentum:
0.01 Nms
Mass:
0.250 Kg
Supply Voltage:
3.3 to 5 V
Power Consumption:
1 W
Space Heritage:
Yes
Operating Temperature:
-20 to 60 Degree C
Interface:
I2C, UART
more info
Description:High Performance Satellite Attitude Control Reaction Wheel for 12-16U Satellite Missions
Satellite Type:
NanoSat, CubeSat
Torque:
Up to 20 mNm
Angular Momentum:
100 mNms
Mass:
350 g
Power Consumption:
1 W
Space Heritage:
Yes
more info
Description:Satellite Reaction Wheel for CubeSat
Satellite Type:
CubeSat
Torque:
0.00023 Nm
Angular Momentum:
0.00058 Nms
Mass:
24 g
Speed:
8000 rpm
Operating Temperature:
-20 to 50 Degree C
more info
Description:3-6U High Production Capacity, Low Disturbance Lightweight Reaction Wheel for 300Kg Class
Satellite Type:
SmallSat
Torque:
100 mNm
Angular Momentum:
2 Nms
Mass:
1.9 Kg
Supply Voltage:
18 to 34 V
Power Consumption:
100 W
Operating Temperature:
-20 to 50 Degree C
Interface:
RS-485
more info
Description:Reaction Wheel for Attitude Control of CubeSats
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:The Bradford Reaction Wheel Unit (RWU) channel consists of a Reaction Wheel Assembly (RWA) and one Wheel Drive Electronics Box (WDE).
Torque:
265 mNm
Angular Momentum:
25 Nms
Mass:
6.02 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:
7 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: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:0.050 Nms Angular Momentum Reaction Wheels with advanced lubrication system for long life and vibration isolation
Torque:
7 mNm
Angular Momentum:
0.050 Nms
Mass:
0.24 Kg
Supply Voltage:
10 to 14 V
Power Consumption:
1 W
Space Heritage:
Yes
Interface:
RS-422
more info
Description:2 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
2 mNm
Angular Momentum:
5.7 mNms
Mass:
115 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:Reaction Wheel for CubeSats
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

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