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MicroSat Reaction Wheels

11 MicroSat Reaction Wheels from 4 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.

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  • Satellite Type: MicroSat
Reaction/Momentum Wheel (RMW) Image
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SITAEL - Reaction/Momentum Wheel (RMW)

MicroSat Reaction Wheel from SITAEL
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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
1Nms RW-1.0 Image
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Rocket Lab - 1Nms RW-1.0

MicroSat Reaction Wheel from Rocket Lab
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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
400 mNms RW-0.4 Image
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400 mNms Reaction Wheel for Science Microsatellites

MicroSat Reaction Wheel from Rocket Lab
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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
60 mNms RW-0.06 Image
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Rocket Lab - 60 mNms RW-0.06

MicroSat Reaction Wheel from Rocket Lab
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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
30 mNms RW-0.03 Image
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Rocket Lab - 30 mNms RW-0.03

MicroSat Reaction Wheel from Rocket Lab
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Description:Vacuum-Lubricated Reaction Wheels Are Designed For Picosatellites, Nanosatellites And Microsats
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 6 V
Power Consumption:
1.8 W
Space Heritage:
Yes
Operating Temperature:
-40 to 70 Degree C
Interface:
UART, I2C, SMBus
more info
10 mNms RW-0.01 Image
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Reaction Wheel for CubeSats

MicroSat Reaction Wheel from Rocket Lab
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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
3 mNms RW-0.003 Image
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Rocket Lab - 3 mNms RW-0.003

MicroSat Reaction Wheel from Rocket Lab
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Description:Vacuum-Lubricated Reaction Wheels Are Designed For Picosatellites, Nanosatellites And Microsats
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
MicroWheel 200 Image
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Miniature Reaction Wheel Torque Actuator for Mini & Micro Satellites

MicroSat Reaction Wheel from Microsat Systems Canada Inc
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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
MicroWheel 1000 Image
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Microsat Systems Canada Inc - MicroWheel 1000

MicroSat Reaction Wheel from Microsat Systems Canada Inc
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Description:Small Satellites Requiring Less Than 1000 mNms Of Momentum Storage For Mini-Satellites And Microsatellites
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
MicroWheel 4000 Image
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Small Satellites Requiring Up To 4 Nms Of Momentum Storage

MicroSat Reaction Wheel from Microsat Systems Canada Inc
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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
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