Preprints
https://doi.org/10.5194/egusphere-2026-1579
https://doi.org/10.5194/egusphere-2026-1579
15 Jun 2026
 | 15 Jun 2026
Status: this preprint is open for discussion and under review for Geoscientific Instrumentation, Methods and Data Systems (GI).

A Cubesat-optimized Magnetic Field Measurement Concept for Operation Beyond Low Earth Orbit

Raphael Steinhöfler, Marius Anger, Roman Shalamov, Jaan Praks, David Fischer, Werner Magnes, Josef Wilfinger, Aris Valavanoglou, and Constant Michel Felix Lentz

Abstract. This paper presents a CubeSat-optimized measurement concept for magnetic field, which was designed for missions beyond low Earth orbit targeting novel radiation belt studies. The instrument combines a miniaturized three-axis fluxgate sensor on a low‑mass deployable boom together with a compact sensor control unit that implements fully synchronous excitation, sampling, and digital control. A hybrid feedback module integrates three prototype fluxgate feedback microchips that provide low‑noise current sources with selectable full‑scale ranges (±3/±9 mA), enabling vector measurements over ±70 μT while retaining sub‑nT resolution. The boom provides 65 cm standoff from the CubeSat and pointing knowledge of 1°. The designed boom length limits the tolerable magnetic dipole moment inside the CubeSat to 0.05 Am2. Extended housekeeping includes voltage supply and thermal monitoring, an additional magneto‑inductive sensor on the sensor control unit for disturbance discrimination, and total ionizing dose tracking. Laboratory characterization demonstrates noise densities of 20–30 pT√Hz at 1 Hz, with 128 vectors per second science data and linearity suitable for near‑Earth fields. As it is a pivotal element in the instrument, the prototype feedback microchip was tested for its radiation response. Heavy‑ion testing showed no single‑event latch‑up up to 100 MeV cm2mg. Single‑event transients as well as single-event upsets were observed and are consistent with rare functional interrupts in the digital part of the signal chain. They are addressable by standard redundancy techniques. X‑ray tests up to 1 Mrad confirm functionality with worst‑case gain and offset drifts of approximately 600 ppmkrad and 1 μAkrad within 0–100 krad. The prototype meets the performance requirements derived from the Foresail‑2 mission concept and demonstrates a path to high‑quality, resource‑efficient magnetometry on 3U–6U CubeSat platforms suitable for operation in the Van Allen belts and other harsh radiation environments.

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Raphael Steinhöfler, Marius Anger, Roman Shalamov, Jaan Praks, David Fischer, Werner Magnes, Josef Wilfinger, Aris Valavanoglou, and Constant Michel Felix Lentz

Status: open (until 21 Jul 2026)

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Raphael Steinhöfler, Marius Anger, Roman Shalamov, Jaan Praks, David Fischer, Werner Magnes, Josef Wilfinger, Aris Valavanoglou, and Constant Michel Felix Lentz
Raphael Steinhöfler, Marius Anger, Roman Shalamov, Jaan Praks, David Fischer, Werner Magnes, Josef Wilfinger, Aris Valavanoglou, and Constant Michel Felix Lentz
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Latest update: 15 Jun 2026
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Short summary
This study investigates concepts of measuring magnetic fields with CubeSats. An exemplary instrument including the sensor, electronics, and boom was designed, built and tested. A novel Application-Specific Integrated Circuit has been used and concepts of larger missions have been adapted. Tests have shown the radiation hardness of the electronics and an improved performance over existing concepts. The results validate the technology and set further directions of CubeSat instrument developments.
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