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YUZHNOYE SDO :: Aerospace Technology :: Aerospace Systems and Components :: Spacecraft Components :: Spacecraft Mechanisms :: magnetoquers

magnetoquers

A magnetorquer is a propulsion element in the magnetic attitude control system of a satellite. It generates a dipole magnetic moment.

The sensor is reliable and does not require maitenance during storage and operation. It is capable of sustaining higher dynamic loads.

As compared to gas-jet nozzles, magnetorquers do not consume any working medium (compressed gas, propellant)


Nominal magnetic moment, Ŕ×ě2 918120350
Nominal consumption power at 27V
supply pressure and 25°C, W
1.61.8515
Mass, kg0.350.53.89.8
Dimensions, mm:
- length
- diameter

170
22

250
22

500
4.2

1000
5.5
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