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arXiv · 2607.06318

Long-term performance of SiPMs in space environment measured by GRBAlpha, GRBBeta, and VZLUSAT-2 CubeSats

Jakub Ripa·Filip Munz·Marianna Dafcikova·Andras Pal·Norbert Werner·Masanori Ohno·Laszlo Meszaros·Balazs Csak·Pavel Kosik·Michaela Duriskova·Lea Szakszonova·Martin Kolar·Tomas Vitek·Nikola Husarikova·Filip Hroch·Michal Pazderka·Yasushi Fukazawa·Hiromitsu Takahashi·Tsunefumi Mizuno·Jean-Paul Breuer·Masato Yokota·Kazuhiro Nakazawa·Hirokazu Odaka·Yuto Ichinohe·Tomas Urbanec·Ales Povalac·Miroslav Kasal·Miroslav Smelko·Peter Hanak·Gabor Galgoczi·Martin Topinka·Hsiang-Kuang Chang·Tsung-Che Liu·Chih-Hsun Lin·Chin-Ping Hu·Che-Chih Tsao·Kaustubha Sen·Chih-En Wu·Jakub Kapus·Jan Hudec·Marcel Frajt·Maksim Rezenov·Vladimir Daniel·Petr Svoboda·Juraj Dudas·Martin Sabol·Ivo Vertat·Robert Laszlo·Martin Koleda
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Abstract

In this work, we report the successful application of silicon photomultipliers (SiPMs) in gamma-ray burst (GRB) detectors used in CubeSats operating in the low Earth orbit (LEO) radiation environment. It is known that SiPMs are susceptible to radiation damage, leading to an increase in the dark count rate. This results in an increase in the low-energy threshold in detectors combining SiPMs and scintillators. Despite this drawback, they became popular in gamma-ray detectors on CubeSats due to their low operating voltage, small size and fast response. Therefore, it is important to characterise their long-term performance in the space environment. Here, we describe the changes in the dark count rate and low-energy threshold of S13360-3050PE multi-pixel photon counters (MPPCs) by Hamamatsu Photonics K.K., using measurements from the GRBAlpha, GRBBeta, and VZLUSAT-2 CubeSats. In the case of GRBAlpha, the measurement of SiPM performance in space lasted over 4 years. GRBAlpha was a 1U CubeSat launched on 2021/03/22 to a 550 km altitude polar orbit carrying a CsI(Tl) scintillator GRB detector employing eight MPPCs and sensitive in the range of ~30-900 keV. GRBAlpha de-orbited on 2025/06/09. VZLUSAT-2 was a 3U CubeSat launched on 2022/01/13 to a 535 km altitude polar orbit and de-orbited on 2025/11/30. GRBBeta was launched on 2024/07/09 to a 580 km altitude, 62° inclination orbit. Both VZLUSAT-2 and GRBBeta carry detectors similar to the one on GRBAlpha. We have flight-proven the Hamamatsu MPPCs S13360-3050 PE and demonstrated that SiPMs, shielded by 2.5 mm of PbSb alloy, can be used in a LEO environment on a scientific mission lasting beyond 4 years. This shows the potential for SiPMs to be employed in future satellites.

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Jakub Ripa, Filip Munz, Marianna Dafcikova, Andras Pal, Norbert Werner, Masanori Ohno, Laszlo Meszaros, Balazs Csak, Pavel Kosik, Michaela Duriskova, Lea Szakszonova, Martin Kolar, Tomas Vitek, Nikola Husarikova, Filip Hroch, Michal Pazderka, Yasushi Fukazawa, Hiromitsu Takahashi, Tsunefumi Mizuno, Jean-Paul Breuer, Masato Yokota, Kazuhiro Nakazawa, Hirokazu Odaka, Yuto Ichinohe, Tomas Urbanec, Ales Povalac, Miroslav Kasal, Miroslav Smelko, Peter Hanak, Gabor Galgoczi, Martin Topinka, Hsiang-Kuang Chang, Tsung-Che Liu, Chih-Hsun Lin, Chin-Ping Hu, Che-Chih Tsao, Kaustubha Sen, Chih-En Wu, Jakub Kapus, Jan Hudec, Marcel Frajt, Maksim Rezenov, Vladimir Daniel, Petr Svoboda, Juraj Dudas, Martin Sabol, Ivo Vertat, Robert Laszlo, Martin Koleda. 2026-07-07. Long-term performance of SiPMs in space environment measured by GRBAlpha, GRBBeta, and VZLUSAT-2 CubeSats. https://doi.org/10.1117/12.3102603

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