About this product

Product information from the supplier.

Products Detail

 

Read More About satellite component

 

Product Code

SC-AOC-MT-102-01-5Am2

SC-AOC-MT-102-02-15Am2

SC-AOC-MT-102-03-100Am2

SC-AOC-MT-102-04-1Am2

Weight

0.275kg

0.7kg

4kg

0.07kg

Envelope Size/mm

228×38×22.8

270×56×30.3

630×80×74

138×32×17

Rated Output Magnetic Moment

5Am2

15Am2

100Am2

1Am2

Residual Magnetic Moment

0.02Am2

0.1Am2

0.1Am2

0.01Am2

Magnetization/Demagnetization Time Constant

70ms

150ms

160ms

50ms

Power Consumption

0.7W

2W

2.7W

0.3W

Supply Cycle

4 months

5 months

5 months

4 months

 

The Magnetic Torque system is a key technology used for attitude control in space applications, such as satellites and spacecraft. It utilizes the Earth's magnetic field to generate torque and control the orientation or attitude of a spacecraft. The system consists of magnetorquers, which are coils placed on the spacecraft's structure. When these coils are energized, they interact with the magnetic field to produce torque, allowing the spacecraft to rotate or stabilize its position. Magnetic torque systems are highly effective in low Earth orbit (LEO), where the Earth's magnetic field is strong enough to be utilized for attitude adjustment without the need for fuel or mechanical moving parts. The system is power-efficient, lightweight, and reliable, making it ideal for small satellites or mission-critical spacecraft that require precision orientation without the complexity of traditional reaction wheels or control moment gyroscopes. Additionally, the system can operate in conjunction with other control mechanisms like reaction wheels to provide redundancy and fine-tuned control.