Space Inventor Magnetorquer
State of the art report 2024
1U and larger satellites

Magnetorquer

Magnetorquer rod for momentum dumping of LEO satellites.

The MT-P4 magnetorquer rod is an integrated solution designed for momentum dumping of LEO satellites. The core is annealed Alloy 79 wound with enameled copper winding and optimized for low power consumption at nominal magnetic dipole of 2 Am2.
 

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GNC

Size

MT-2-P4
MT-6-P4

MSRP

€6.000

Specifications

Description

Magnetorquer rod for momentum dumping of LEO satellites.

The MT-P4 magnetorquer rod is an integrated solution designed for momentum dumping of LEO satellites. The core is annealed Alloy 79 wound with enameled copper winding and optimized for low power consumption at nominal magnetic dipole of 2 Am2. The MT-P4 has built-in control electronics and is simply interfaced by 28V unregulated battery voltage and redundant CAN busses. The MT-P4 comprises redundant input supply connected using diodes, redundant torquerrod windings and redundant driver electronics for enhanced reliability. The mounting brackets can be moved to accommodate various mounting features on the satellite bus.

Features

Nominal Dipole Moment
2 Am2
Power Consumption
250 mW
Mass
375 g
Rod Dimensions
Ø17 mm x 200 mm
Redundant input supply, driver electronics, and windings
Magnetorquer rod with integrated controller
Interface: Redundant CAN with CSP 2.0 protocol
Low residual dipole

Mechanical drawing

Space Inventor Magnetorquer Blueprint

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