Reaction Wheels - Page 7

113 Reaction Wheels from 31 Manufacturers meet your specification.
Description:16 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
16 mNm
Angular Momentum:
50 mNms
Mass:
310 g
Speed:
10000 rpm
Vibration:
14.16 g RMS
Dynamic Imbalance:
0.05 g.cm²
Supply Voltage:
6.4 to 16.8 V (Motor Supply Voltage)
Power Consumption:
800 to 5300 mW(Average Power)
Space Heritage:
Yes
Operating Temperature:
-20 to 80 Degree C(Thermal vacuum)
Interface:
CAN, UART, RS-485
more info
Description:1U CubeSat Reaction Wheel
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
±1 mNm
Angular Momentum:
0.003 Nms (Nominal), 0.005 Nms (Peak)
Mass:
0.05 Kg
Vibration:
14 g RMS
Supply Voltage:
4.5 to 9 V
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
UART, I2C, SMBus
more info
Description:2 Nms Angular Momentum Reaction Wheels for Satellite Constellations
Torque:
±50 mNm
Angular Momentum:
2 Nms
Mass:
2 Kg
Speed:
±6000 rpm
Vibration:
26 g RMS random 3 axis
Static Imbalance:
3 g-cm
Dynamic Imbalance:
10 g-cm2
Supply Voltage:
28 to 47 V
Power Consumption:
65 W
Space Heritage:
Yes
Storage Temperature:
-40 to 80 Degree C
Operating Temperature:
-20 to 70 Degree C
Interface:
RS-422, RS-485, CAN
more info
Description:Plug-&-Play, Radiation Proof, Reaction Wheel With A Long Life Time, Safeguarded Electronics, And A Very Compact Design
Torque:
8 mNm
Angular Momentum:
0.06 Nms, 0.08 Nms
Mass:
0.3 Kg
Supply Voltage:
12 to 16 V
Power Consumption:
0.07 to 0.5 W
Operating Temperature:
-25 to 45 Degree C
Interface:
RS-485
more info
Description:Small Satellite Class Reaction Wheel Assembly
Satellite Type:
SmallSat
Torque:
200 mNm
Angular Momentum:
11.5 Nms
Mass:
5.5 Kg
Supply Voltage:
28 V
Power Consumption:
5 W
Space Heritage:
Yes
Operating Temperature:
-10 to 50 Degree C
Interface:
RS-422
more info
Description:RS400 Reaction Sphere
Satellite Type:
CubeSat
Torque:
4 mNm
Angular Momentum:
0.02 Nms
Mass:
1 Kg
Supply Voltage:
3.3 to 5 V
Power Consumption:
4 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 Satellite Missions
Torque:
Up to 100 mNm
Angular Momentum:
500 mNms
Mass:
800 g
Power Consumption:
3 W
Space Heritage:
Yes
more info
Description:Spacecraft Reaction Wheel for LEO Missions
Torque:
11 mN.m
Angular Momentum:
1.5 Nms
Mass:
2.6 Kg
Speed:
±5000 rpm
Vibration:
5 to 8.5 g RMS
Static Imbalance:
0.2 g-cm
Dynamic Imbalance:
0.4 g-cm2
Supply Voltage:
24.1 to 35 V
Power Consumption:
1.2 to 113 W
Storage Temperature:
-30 to 60 Degree C
Operating Temperature:
-20 to 50 Degree C
Interface:
RS-422, CAN
more info
Description:Reaction Wheel for CubeSats
Satellite Type:
Cubesat, SmallSat
Torque:
0.002 Nm
Angular Momentum:
0.03 Nms
Mass:
0.2 Kg
Speed:
5000 to 5500 rpm
Supply Voltage:
5 V
Power Consumption:
1.5 to 2.8 W
Operating Temperature:
-20 to 50 Degree C
Interface:
CAN, SPI
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

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