Magnetic Torquer

The Magnetic Torquer delivers a dipole moment of 1 A·m² for effective spacecraft attitude control using Earth's magnetic field. The modular, low-power design is scalable and can be customized for missions ranging from CubeSats to small satellites up to a 150 kg class bus, ensuring reliable integration with modern ADCS architectures.

Capabilities

Key Features

  • Dipole moment: 1 A·m²
  • Modular, low-power design
  • Scalable for CubeSats to 150 kg satellites
  • Seamless ADCS integration
  • Customizable for mission requirements
  • Radiation-hardened electronics
  • Temperature-compensated design
  • Lightweight construction
Magnetic Torquer

Applications

  • Spacecraft attitude control
  • Momentum management
  • CubeSat & NanoSat missions
  • Small satellite platforms (up to 150 kg)
  • ADCS (Attitude Determination & Control Systems)
  • Detumbling operations

Specifications

  • Type: Magnetic Torquer Rod
  • Dipole Moment: 1 A·m²
  • Platform Compatibility: CubeSats, NanoSats, Small Satellites (up to 150 kg)
  • Power: Low-power design
  • Integration: ADCS compatible
  • Design: Modular & Customizable