Reaction Wheels - Page 6

113 Reaction Wheels from 31 Manufacturers meet your specification.
Description:Plug-&-Play, Radiation Proof, Reaction Wheel With A Long Life Time, Safeguarded Electronics, And A Very Compact Design
Torque:
4 mNm
Angular Momentum:
0.04 Nms, 0.06 Nms
Mass:
0.26 Kg
Supply Voltage:
12 to 16 V
Power Consumption:
0.07 to 0.5 W
Operating Temperature:
-25 to 45 Degree C
Interface:
RS-485
more info
Description:30 mNm Torque Reaction Wheel Assembly for Small Satellites
Satellite Type:
SmallSat
Torque:
30 mNm
Angular Momentum:
1 Nms
Mass:
2.6 Kg
Speed:
9000 rpm
Vibration:
16 g RMS
Static Imbalance:
1.3
Dynamic Imbalance:
13 g-cm2
Supply Voltage:
28 V
Power Consumption:
25 W
Space Heritage:
Yes
Operating Temperature:
-10 to 60 Degree C
Interface:
RS-422, CAN, LVDS, CMOS
more info
Description:Miniature Reaction Wheel Torque Actuator for 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
Description:6.26 to 7.83 Nms Angular Momentum extensive in-orbit heritage Reaction Wheel for longer lifetime missions and constellation programmes
Satellite Type:
SmallSat
Torque:
200 mNm, 300 mNm (Peak)
Angular Momentum:
6.26 to 7.83 Nms
Mass:
5 Kg
Speed:
5000 rpm
Vibration:
14 g RMS
Supply Voltage:
28 V
Power Consumption:
6 to 136 W
Space Heritage:
Yes
Operating Temperature:
-20 to 60 Degree C
Interface:
RS-485
more info
Description:Fully Integrated Reaction Wheel Unit for High Performance Satellite Attitude Control Satellite Missions
Torque:
Up to 1 Nm
Angular Momentum:
1 Nms
Mass:
1.2 Kg
Power Consumption:
3 W
Space Heritage:
Yes
more info
Description:Space Satellite Vehicle
Torque:
11 mN.m
Angular Momentum:
1.5 Nms
Mass:
2.6 Kg
Speed:
±5000 rpm
Vibration:
11 g RMS
Static Imbalance:
0.2 g-cm
Dynamic Imbalance:
0.4 g-cm2
Supply Voltage:
24.1 to 35 V
Power Consumption:
1.2 to 113 W
Storage Temperature:
-30 to 60 Degree C
Operating Temperature:
-20 to 50 Degree C
Interface:
RS-422, CAN
more info
Description:0.35 Nms Reaction Wheel for SmallSats
Satellite Type:
SmallSat
Torque:
0.015 nNm
Angular Momentum:
0.35 Nms
Mass:
0.9 Kg
Speed:
6000 to 7800 rpm
Operating Temperature:
-20 to 50 Degree C
more info
Description:3-6U High Production Capacity, Low Disturbance Lightweight Reaction Wheel for 200Kg Class
Satellite Type:
MiniSat
Torque:
100 mNm
Angular Momentum:
1 Nms
Mass:
1.5 Kg
Supply Voltage:
18 to 34 V
Power Consumption:
100 W
Operating Temperature:
-20 to 50 Degree C
Interface:
RS-485
more info
Description:Small Satellite missions high reliability, adaptability, and accuracy Reaction Wheels
Torque:
47.1 mN.m
Angular Momentum:
±1.2 Nms
Mass:
1.5 Kg
Speed:
6500 rpm
Vibration:
10 g RMS
Supply Voltage:
20 to 34 V
Power Consumption:
24 W
Space Heritage:
Yes
Storage Temperature:
-40 to 85 Degree C
Operating Temperature:
-10 to 50 Degree C
more info
Description:The Bradford Reaction Wheel Unit (RWU) channel consists of a Reaction Wheel Assembly (RWA) and one Wheel Drive Electronics Box (WDE).
Torque:
248 mNm
Angular Momentum:
40 Nms
Mass:
6.7 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:
8 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

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