4.6 Article

Characterization of Silicon Photomultipliers (SiPMs) for Space Exploration

Journal

ADVANCES IN SPACE RESEARCH
Volume 70, Issue 11, Pages 3750-3768

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.asr.2022.08.047

Keywords

Silicon photomultiplier; SiPM; Quenching resistor; Breakdown voltage; Space exploration of SiPMs; Accelerated temperature test

Funding

  1. Department of Space, Government of India

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This article introduces the characterization and response of Silicon Photomultipliers (SiPMs) in hardened environments. Two experiments were conducted to test the electrical characteristics of SiPMs from different manufacturers and to evaluate their performance in simulated space conditions.
Silicon Photomultipliers (SiPMs) are the devices, which along with scintillation detectors can be used for the radiation measurements. We are developing instruments using scintillation detector and SiPM arrays for the measurements of high-energy X-rays and charged particles. These instruments are being developed for the future space exploration programs. Here, we report the work carried out for the characterization of SiPM and its response in the hardened environments. Results from two different experiments are presented. In the first experiment: electrical characterizations of SiPMs from two manufacturers i.e. SensL (now Onsemi) and Ketek have been car-ried out. Three different pixel sizes 20 lm, 35 lm and 50 lm of MicroC series from SensL and 50 lm pixel size of PM3350 series of Ketek have been tested. In order to see 'device - to -device' variations, three SiPMs of each pixel size are used in the experiment i.e. total twelve SiPMs have been characterized for the breakdown voltage, quenching resistor and their temperature dependences. Variations in the gain and microcell recovery time due to temperature are also estimated. In the second experiment: one of the SiPM models (SensL make 35 lm pixel size) has been subjected to various environmental tests mimicking the space conditions. Matching of pre and post I-V mea-surements for each tests confirms that performance of the device is not degraded and hence selected model of SiPM can be explored for the future space instrumentation.(c) 2022 COSPAR. Published by Elsevier B.V. All rights reserved.

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