NanoSat Reaction Wheels

13 NanoSat Reaction Wheels from 7 Manufacturers meet your specification.

NanoSat 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: NanoSat
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
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:0.5 Nms Reaction Wheels Serving micro satellite missions with a minimum of 5 years lifetime
Satellite Type:
NanoSat, MicroSat, SmallSat
Torque:
50 to 100 mNm
Angular Momentum:
0.5 Nms
Mass:
0.850 Kg
Power Consumption:
3.5 W
Space Heritage:
Yes
more info
SKU:cyber reaction wheel 2
Satellite Type:
PicoSat, NanoSat
Torque:
0.4 mNm (Peak)
Angular Momentum:
0.002 Nms
Mass:
0.03 Kg
Speed:
18000 rpm
Supply Voltage:
5V
Power Consumption:
0.48 W
Storage Temperature:
-60 to 100 Degree C
Operating Temperature:
-40 to 85 Degree C
Interface:
UART, I2C, SPI
more info
SKU:NanoTorque GSW-600
Satellite Type:
NanoSat, CubeSat
Torque:
1.5 mNm
Angular Momentum:
0.019 Nms
Mass:
0.180 Kg (One Wheel), 0.940 Kg (Pyramid)
Speed:
-6000 to 6000 rpm
Supply Voltage:
5 V
Storage Temperature:
-40 to 85 Degree C
Operating Temperature:
-40 to 80 Degree C
Interface:
CAN, I2C, SPI
more info
SKU:3 mNms RW-0.003
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:0.042 Nms Reaction Wheels Serving micro satellite missions with a minimum of 5 years lifetime
Satellite Type:
NanoSat, SmallSat
Torque:
5 mNm
Angular Momentum:
0.042 Nms
Mass:
0.155 Kg
Power Consumption:
0.35 W
Space Heritage:
Yes
more info
SKU:RW1 Type B
Satellite Type:
CubeSat, NanoSat
Torque:
4 Nm
Angular Momentum:
1 Nms
Mass:
1200 Kg
Speed:
8000 to 16, 380 rpm
Operating Temperature:
-20 to 50 Degree C
more info
Description:Vacuum-Lubricated Reaction Wheels Are Designed For Picosatellites, Nanosatellites And Microsats
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
100 mNm
Angular Momentum:
1 Nms
Mass:
1.38 Kg
Vibration:
14 g RMS
Supply Voltage:
24 to 34 V
Power Consumption:
43 W
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
RS-485
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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