SAVomid reaction wheel is installed on the satellite and by combining the speed of reaction wheels, the satellite can be rotated around three axes or a combination of these three axes. Commands for each of the wheels installed on the satellite are sent by the command center to the satellite receiver and applied to the wheels via the internal network. The reaction wheel actuator is mainly used to control the status of the satellite. These actuators are able to provide the torque and momentum required to maneuver and stabilize the satellite.
Reaction wheel SAV-ARW110
Out of stock
- SAVomid reaction wheel is a type of engine pancakes (engines with very low height and compression).
- It has a high efficiency of 98%. This has led to much lower power consumption than similar types.
Momentum 0.5 Nms
Max Torque 10 / 25 mN.m
Torque @ Half Momentum 0.0125 Nm
Life Time >3 Years
Mass =< 0.95 Kg
Power @ Standby 3W
Power @ Full Momentum 8W
Power @ Max Torque 40W
Data Interface RS-485/RS-422/CAN
Operating Temperature -20 °C to +60 °C
Storage Temperature -35°C to +85 °C
Fine Dynamic Imbalance – Statice =< 0.35 g.cm
Fine Dynamic Imbalance – Couple =< 1.8 g.cm2
- Current (Optional)
- Voltage (Optional)