Space Weather Magnetometer Aboard GEO-KOMPSAT-2A
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Space Weather Magnetometer Aboard GEO-KOMPSAT-2A W. Magnes1 · O. Hillenmaier2 · H.-U. Auster3 · P. Brown4 · S. Kraft5 · J. Seon6 · M. Delva1 · A. Valavanoglou1 · S. Leitner1 · D. Fischer1 · G. Berghofer1 · Y. Narita1 · F. Plaschke1 · M. Volwerk1 · J. Wilfinger1 · C. Strauch2 · J. Ludwig2 · D. Constantinescu3 · K.-H. Fornacon3 · K. Gebauer3 · D. Hercik3 · I. Richter3 · J.P. Eastwood4 · J.P. Luntama5 · A. Hilgers5 · M. Heil5 · G.W. Na6 · C.H. Lee6 Received: 3 June 2020 / Accepted: 27 September 2020 © The Author(s) 2020
Abstract The South Korean meteorological and environmental satellite GEO-KOMPSAT2A (GK-2A) was launched into geostationary orbit at 128.2◦ East on 4 December 2018. The space weather observation aboard GK-2A is performed by the Korea Space Environment Monitor. It consists of three particle detectors, a charging monitor and a four-sensor Service Oriented Spacecraft Magnetometer (SOSMAG). The magnetometer design aims for avoiding strict magnetic cleanliness requirements for the hosting spacecraft and an automated on-board correction of the dynamic stray fields which are generated by the spacecraft. This is achieved through the use of two science grade fluxgate sensors on an approximately one meter long boom and two additional magnetoresistance sensors mounted within the spacecraft body. This paper describes the instrument design, discusses the ground calibration methods and results, presents the post-launch correction and calibration achievements based on the data which were acquired during the first year in orbit and demonstrates the in-flight performance of SOSMAG with two science cases. The dynamic stray fields from the GK-2A spacecraft, which was built without specific magnetic cleanliness considerations, are reduced up to a maximum factor of 35. The magnitude of the largest remnant field from an active spacecraft disturber is 2.0 nT. Due to a daily shadowing of the SOSMAG boom, sensor intrinsic offset oscillations with a periodicity up to 60 minutes and peak-to-peak values up to 5 nT remain in the corrected data product. The comparison of the cleaned SOSMAG data with the Tsyganenko 2004 magnetic field model and the magnetic field data from the Magnetospheric Multiscale mission demon-
B W. Magnes 1
Space Research Institute, Austrian Academy of Sciences, Graz, Austria
2
Magson GmbH, Berlin, Germany
3
Institut für Geophysik und extra-terrestrische Physik, Technische Universität Braunschweig, Braunschweig, Germany
4
Blackett Laboratory, Imperial College London, London, UK
5
European Space Agency, Paris, France
6
School of Space Research, Kyung Hee University, Suwon, Korea
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strates that the offset error is less than the required 5 nT for all three components and that the drift of the offsets over 10 months is less than 7 nT. Future work will include a further reduction of the remaining artefacts in the final data product with the focus on lessening the temperature driven sensor oscillations with an epoch based identification and correction. Keywords Space
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