PicoSat Reaction Wheels

7 PicoSat Reaction Wheels from 2 Manufacturers meet your specification.

PicoSat 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: PicoSat
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: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: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: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
SKU:400 mNms RW-0.4
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
100 mNm
Angular Momentum:
0.4 Nms
Mass:
0.77 kg
Vibration:
14 g RMS
Supply Voltage:
24 to 34 V
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
RS-485
more info
Description:Vacuum-Lubricated Reaction Wheels Are Designed For Picosatellites, Nanosatellites And Microsats
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
±20 mNm
Angular Momentum:
0.06 Nms (Nominal), 0.18 Nms (Peak)
Mass:
0.226 Kg
Vibration:
23 g RMS
Supply Voltage:
7.5 to 34 V
Power Consumption:
23.4 W
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
RS-485, CAN
more info
SKU:30 mNms RW-0.03
Satellite Type:
NanoSat, MicroSat, PicoSat
Torque:
±0.5 to ±2 mNm
Angular Momentum:
0.03 Nms (Nominal), 0.04 Nms (Peak)
Mass:
0.185 Kg
Vibration:
12 g RMS
Supply Voltage:
3.4 to 8 V
Power Consumption:
0 to 1.8 W
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
UART, I2C, SMBus
more info

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Angular Momentum (Nms)

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Radiation Tolerance (krad)

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Supply Voltage (V)

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Space Heritage

Interface