- Main Features
- Documents
Active damping for spin stabilized, momentum biased and gravity gradient controlled CubeSats
Momentum dumping of reaction wheels in three axis stabilized spacecraft
More than 150 rods delivered to CubeSat programmes over the last 8 years.
Low cost standard product
High moment for low power
Small size and low mass
Simple interface
No residual magnetic moment
Lifetime: >10 years
Dimensions: 70mm (length) x 9 mm (diameter)
Overall Diameter: < 9 mm
Mounting: tied and bounded direct to PCB
Mass: < 30 g
Interfaces: Coil wires solder direct to PCB pads
Operating range: -35°C to +75°C
NSS CubeSat Magnetorquer Rod
Magnetorquers offer a method of controlling the attitude of a spacecraft. This can be achieved either directly, by interacting with the local Earth’s magnetic field, or in combination with reaction wheels where they allow a method of dumping excess momentum in the wheels without the need for a complex propulsion system.
The use of a magnetic alloy rod produces an amplification effect over an air cored magnetorquer. This allows a system that uses less power, which is critical for CubeSat missions. The rods can enable a mission with increased manoeuvrability and reduced detumble rates.
CubeSat Magnetorquer rods are designed to be run directly from a switched 5 Volt power output from the on-board power control system.
Main Features
Application:
Testing & Heritage:
Features:
Properties
Related products
- About ByHEAD
- Contact Us
- Privacy Policy
- Terms & Conditions
Copyright © 2016 China Head Aerospace Technology Co. All Rights Reserved Statistics