Summary

The NewSpace Systems (NSS) NCTR-M016 Magnetorquer Rod can be used for spacecraft attitude control. NSS' magnetorquer rod designs are TRL 9 and have extensive in-orbit heritage. Some of the larger NSS magnetorquer rods were first flown in 2014 on the SaudiSat-4 and DX-1 missions. Since then, NSS has become one of the largest magnetorquer rod manufacturers in the world, having delivered more than 200 CubeSat Rods and 1000 MicroSat Rods to a variety of international missions and constellations, all with differing performance requirements. To date, NSS magnetorquers have been baselined on three international constellations.

Magnetorquers offer a method of controlling the attitude of a spacecraft either directly, by interacting with the local Earth's magnetic field or, more usually, in combination with reaction wheels. This secondary method allows for the dumping of excess momentum in the reaction wheels without the need for a complex propulsion system.

The NSS magnetorquer rods use a magnetic alloy rod which produces an amplification effect over an air cored magnetorquer. This allows a system that uses less power and is less susceptible to magnetic torque variations due to temperature.

Each rod is typically bifilar wound for redundancy, or the windings can be activated together to increase the torque produced. While drive circuits for the rods can be supplied if required, they typically run directly between a switched power output and the on-board power control system.

Key features of the NSS magnetorquers include:

  • High moment for low power
  • Small size and low mass
  • Small residual magnetic moment
  • Adaptable for size, moment and power to meet optimal system requirements
  • Redundant windings available
  • Simple interface

NSS magnetorquers can be utilized for the following applications:

  • Active damping for spin stabilised, momentum-biased and gravity-gradient-controlled satellites
  • Momentum dumping of reaction wheels in three-axis stabilised spacecraft
  • Simple magnetic stabilisation

All FM parts undergo random vibration (10 rms) as well as thermal cycling (four cycle ambiant pressure) to five degrees beyond operational thermal specifications. NSS can perform additional environmental testing if required by a client.

Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.

Last updated: 2022-11-01

NCTR-M016 Magnetorquer Rod

9TRL

Downloads

Specs

mass
< 53 g
length
107 mm
70 mm (excluding connector)
width
15 mm
height
13 mm
magnetic moment
1.6 Am2 (nominal)
linearity
< ±5% across operating range
residual moment
0.01 Am2
power
< 1.2 W @ 5V (nominal)
power supply
5 V DC
thermal (acceptance)
-25 to 70 C
mechanical vibration
21.06 gRMS (random)
connector type
Molex® Pico-Lock

Export

from our blog

Go to blog

Magnetorquers: an overview of magnetic torquer products available on the global marketplace for space

Find a launch option for your CubeSat or small satellite - an overview of launch service providers

Smallsat and CubeSat GPS antennas and GNSS systems