Science Magnetometer (Space Payload Fluxgate Magnetometer)
Space-qualified tri-axial fluxgate magnetometer used as a scientific payload instrument on spacecraft missions.
Technical specifications
- Sensor type
- Tri-axial vector-compensated fluxgate (ringcore, dual crossed ringcores)
- Noise level
- < 15 pT/sqrt(Hz) @ 1 Hz
- Long-term stability
- Offset drift < 3 nT/year
- Feedback coil material
- Copper and aluminum (matched ~20 ppm/K thermal expansion)
- Signal processing
- FPGA-based instrument control and digital data processing
- Interface
- Serial interface (default), customizable protocols on request
- Qualification
- Fully space-qualified components, ECSS-compliant qualification
- Flight heritage
- BepiColombo, JUICE, Rosetta Lander, Venus Express, Themis, Double Star, MASCOT/Hayabusa2
About
Magson’s Science Magnetometer is a high-performance, space-qualified fluxgate magnetometer instrument designed for use as a scientific payload on spacecraft. It has been designed, manufactured, and qualified in accordance with common space standards (ECSS) to satisfy demanding mission requirements and constraints. The instrument is built around a vector-compensated ringcore sensor with three pickup coil pairs for the X, Y, and Z components, plus a compensating feedback coil system, ensuring temperature-independent axis alignment and long-term measurement stability. Excitation circuitry, preamplifier, feedback current sources, and precision ADC/DAC electronics are combined with FPGA-based digital signal processing. Magson science magnetometers have flown on numerous ESA, DLR, and international missions including BepiColombo (MMO/MPO), JUICE (JMAG-IB), Rosetta Lander, Venus Express, Themis, Double Star, and MASCOT on Hayabusa2, providing precise magnetic field vector measurements for planetary and heliophysics science.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.