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Reaction Wheels - Page 8

113 Reaction Wheels from 31 Manufacturers meet your specification.
W18E Image
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Bradford Space - W18E

Reaction Wheel from Bradford Space
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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:
22 Nms
Mass:
5.65 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:
6 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
RW4 Image
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Blue Canyon Technologies - RW4

Reaction Wheel from Blue Canyon Technologies
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Description:4 Nms Angular Momentum Reaction Wheels with advanced lubrication system for long life and vibration isolation
Torque:
250 mNm
Angular Momentum:
4 Nms
Mass:
3.2 Kg
Supply Voltage:
22 to 34 V
Power Consumption:
10 W
Space Heritage:
Yes
Interface:
RS-422
more info
CW5000 Image
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CubeSpace - CW5000

Reaction Wheel from CubeSpace
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Description:37 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
37 mNm
Angular Momentum:
500 mNms
Mass:
970 g
Speed:
10000 rpm
Vibration:
14.16 g RMS
Dynamic Imbalance:
0.05 g.cm²
Supply Voltage:
16 to 36 V (Motor Supply Voltage)
Power Consumption:
2700 to 9000 mW(Average Power)
Space Heritage:
Yes
Operating Temperature:
-20 to 80 Degree C(Thermal vacuum)
Interface:
CAN, UART, RS-485
more info
60 mNms RW-0.06 Image
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Rocket Lab - 60 mNms RW-0.06

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
VRW-A-05 Image
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VECTRONIC Aerospace GmbH - VRW-A-05

Reaction Wheel from VECTRONIC Aerospace GmbH
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Description:0.69 Nms Angular Momentum Reaction Wheels for Satellite Constellations
Angular Momentum:
0.69 Nms
Mass:
1.3 Kg
Space Heritage:
Yes
Interface:
RS-422, RS-485, CAN
more info
NRWA-T2 Image
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NewSpace Systems - NRWA-T2

Reaction Wheel from NewSpace Systems
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Description:1.41 to 1.63 Nms Angular Momentum extensive in-orbit heritage Reaction Wheel for longer lifetime missions and constellation programmes
Satellite Type:
SmallSat
Torque:
90 mNm
Angular Momentum:
1.41 to 1.63 Nms
Mass:
2.8 Kg
Speed:
2600 to 3000 rpm
Vibration:
16.95 g RMS
Supply Voltage:
28 V
Power Consumption:
1.7 to 4.62 W
Space Heritage:
Yes
Operating Temperature:
-10 to 58 Degree C
Interface:
RS-422
more info
WHL-200-P4 Image
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Space Inventor - WHL-200-P4

Reaction Wheel from Space Inventor
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Description:25 mNm Momentum Wheel for Microsatellites
Satellite Type:
MicroSat
Torque:
25 mNm
Angular Momentum:
200 mNms
Mass:
430 g
Speed:
12000 rpm
Supply Voltage:
9 to 33.6 V
Operating Temperature:
-40 to 60 Degree C
Interface:
CAN, RS-422
more info
RWP015 Image
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Blue Canyon Technologies - RWP015

Reaction Wheel from Blue Canyon Technologies
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Description:Reaction Wheel for LEO Orbit & Deep Space Applications
Torque:
4 mNm
Angular Momentum:
0.015 Nms
Mass:
0.13 Kg
Supply Voltage:
10 to 14 V
Power Consumption:
1 W
Space Heritage:
Yes
more info
CW2500 Image
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CubeSpace - CW2500

Reaction Wheel from CubeSpace
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Description:27 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
27 mNm
Angular Momentum:
250 mNms
Mass:
750 g
Speed:
10000 rpm
Vibration:
14.16 g RMS
Dynamic Imbalance:
0.05 g.cm²
Supply Voltage:
16 to 36 V (Motor Supply Voltage)
Power Consumption:
2700 to 9000 mW(Average Power)
Space Heritage:
Yes
Operating Temperature:
-20 to 80 Degree C(Thermal vacuum)
Interface:
CAN, UART, RS-485
more info
30 mNms RW-0.03 Image
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Rocket Lab - 30 mNms RW-0.03

Reaction Wheel from Rocket Lab
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Description:Reaction Wheel for 6-12U CubeSats
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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