EPSC Abstracts
Vol. 18, EPSC-DPS2025-446, 2025, updated on 09 Jul 2025
https://doi.org/10.5194/epsc-dps2025-446
EPSC-DPS Joint Meeting 2025
© Author(s) 2025. This work is distributed under
the Creative Commons Attribution 4.0 License.
 L-MAG: a temperature-stabilized fluxgate magnetometer system for lunar surface observatories 
Hao Cao1, Krishan Khurana1, Robert Strangeway1, Ryan Caron1, Emil McDowell1, Ryan Seaton1, Henry Gonzalez1, David Pierce2, David Hinkley3, and Natalie Walsh3
Hao Cao et al.
  • 1Department of Earth, Planetary, and Space Sciences, University of California, Los Angeles (UCLA), Los Angeles, CA 90095, USA (hcao@epss.ucla.edu)
  • 2AVARA Magnetics, Las Vegas, NV 89117, USA
  • 3The Aerospace Corporation, El Segundo, CA 90245, USA

Lunar magnetic field investigation connects the interior, the surface, and the space environment of the Moon. Measuring and understanding the lunar magnetic field at different length-scales and time-scales is of critical importance to understand the bulk water content and temperature profile in the lunar mantle, the existence and properties of a partial melt layer above the lunar core, the size of the lunar core, the origin and distribution of volatiles on the lunar surface, and the origin and properties of the past lunar dynamo, all of which are intimately connected to the origin of the Earth-Moon system and the subsequent thermal-chemical-environmental evolution of the Moon. The surface of the Moon, however, is a challenging environment, including contrasting temperatures between lunar day and lunar night, dust, and surface charging.

Here we report our progress in the designing, building, and testing of a temperature-stabilized fluxgate magnetometer (FGM) system for long-term operations on the surface of the Moon. The sensor design draws heritage from those onboard the NASA Magnetospheric Multiscale (MMS) mission, InSight Mars Lander, and the Europa Clipper mission. We refer to this FGM system configuration as L-MAG. One of the key improvements is a magnetically clean heater system that is integrated with the FGM sensor. It is designed to yield a temperature stability of 0.2 degrees C around two set-point temperatures with minimal power consumption. The collocation of the heater with the sensor drastically reduces the necessary heater power. This power efficient FGM design will be compatible with installation onto a lunar lander or placed on the surface of the moon by an astronaut. Our L-MAG system will significantly improve measurement capabilities for upcoming lunar science missions including those via the Commercial Lunar Payload Services (CLPS) and via Artemis astronaut deployments.

How to cite: Cao, H., Khurana, K., Strangeway, R., Caron, R., McDowell, E., Seaton, R., Gonzalez, H., Pierce, D., Hinkley, D., and Walsh, N.:  L-MAG: a temperature-stabilized fluxgate magnetometer system for lunar surface observatories , EPSC-DPS Joint Meeting 2025, Helsinki, Finland, 7–12 Sep 2025, EPSC-DPS2025-446, https://doi.org/10.5194/epsc-dps2025-446, 2025.