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Reaction Wheels - Page 4

113 Reaction Wheels from 31 Manufacturers meet your specification.
DP-DMCS-7000 Image
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Data Patterns (India) Ltd. - DP-DMCS-7000

Reaction Wheel from Data Patterns (India) Ltd.
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Description:Flight Qualified, Compact, Standalone Actuator Unit designed for Cube & Nano Satellite Missions
Satellite Type:
NanoSat, CubeSat
Angular Momentum:
30 mNms
Space Heritage:
Yes
Interface:
I2C
more info
W18 Image
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Bradford Space - W18

Reaction Wheel from Bradford Space
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Description:Reaction Wheel Unit for Satellites
Torque:
265 mNm
Angular Momentum:
18 Nms
Mass:
5.2 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:
5 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
RW1 Image
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Blue Canyon Technologies - RW1

Reaction Wheel from Blue Canyon Technologies
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Description:1 Nms Angular Momentum Reaction Wheels with advanced lubrication system for long life and vibration isolation
Torque:
70 mNm
Angular Momentum:
1 Nms
Mass:
0.95 Kg
Supply Voltage:
22 to 34 V
Power Consumption:
10 W
Space Heritage:
Yes
Interface:
RS-422
more info
CW0162 Image
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CubeSpace - CW0162

Reaction Wheel from CubeSpace
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Description:7 mNm CubeSat Reaction Wheel
Satellite Type:
CubeSat
Torque:
7 mNm
Angular Momentum:
16.2 mNms
Mass:
144 g
Speed:
10000 rpm
Vibration:
14.16 g RMS
Dynamic Imbalance:
0.014 g.cm²
Supply Voltage:
6.4 to 16.8 V (Motor Supply Voltage)
Power Consumption:
336 to 770 mW(Average Power)
Space Heritage:
Yes
Operating Temperature:
-20 to 80 Degree C(Thermal vacuum)
Interface:
CAN, UART, RS-485
more info
RW4-12.0 Image
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Rocket Lab - RW4-12.0

Reaction Wheel from Rocket Lab
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Description:12.0 Nms RWA RW4 Rad-Hard Reaction Wheel
Satellite Type:
SmallSat, NanoSat, MicroSat
Torque:
0.2 Nm
Angular Momentum:
12 Nms
Mass:
5 Kg
Vibration:
16.7 to 20 g RMS
Static Imbalance:
26.7 g-mm
Dynamic Imbalance:
800 g.mm²
Supply Voltage:
24 to 34 V
Power Consumption:
38 to 170 W
Space Heritage:
Yes
Storage Temperature:
-40 to 70 Degree C
Operating Temperature:
-20 to 60 Degree C
Interface:
RS-485
more info
SXC-FW4-02 Image
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SPUTNIX - SXC-FW4-02

Reaction Wheel from SPUTNIX
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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
VRW-D-16 Image
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VECTRONIC Aerospace GmbH - VRW-D-16

Reaction Wheel from VECTRONIC Aerospace GmbH
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Description:1.6 Nms Angular Momentum Reaction Wheels for Satellite Constellations
Angular Momentum:
1.6 Nms
Mass:
1.8 Kg
Space Heritage:
Yes
Interface:
RS-422, RS-485, CAN
more info
RW40 Image
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Comat - RW40

Reaction Wheel from Comat
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Description:4 mNm Reaction Wheels for NanoSatellites
Satellite Type:
NanoSat, SmallSat
Torque:
4 mNm
Angular Momentum:
40 mNms
Mass:
230 g
Speed:
Down to 2 rpm
Supply Voltage:
10 to 18 V
Operating Temperature:
-30 to 50 Degree C(Thermal Qualification)
Interface:
RS-485
more info
MicroWheel 4000 Image
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Microsat Systems Canada Inc - MicroWheel 4000

Reaction Wheel from Microsat Systems Canada Inc
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Description:Small Satellites Requiring Up To 4 Nms Of Momentum Storage
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
NRWA-T065 Image
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NewSpace Systems - NRWA-T065

Reaction Wheel from NewSpace Systems
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Description:0.65 Nms Angular Momentum extensive in-orbit heritage Reaction Wheel for longer lifetime missions and constellation programmes
Satellite Type:
SmallSat
Torque:
200 mNm
Angular Momentum:
0.65 to 0.94 Nms
Mass:
1.55 Kg
Speed:
9000 rpm
Vibration:
16.95 g RMS
Supply Voltage:
28 V
Power Consumption:
2.6-6 W
Space Heritage:
Yes
Operating Temperature:
-10 to 45 Degree C
Interface:
RS-422
more info
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