The ground calibration of the HERMES-Pathfinder payload flight models

TL;DR

This paper details the calibration process of the HERMES-Pathfinder payloads, demonstrating their spectroscopic performance and limitations for gamma-ray burst detection using miniaturized instruments on nano-satellites.

Contribution

It presents the ground calibration procedures and results for the HERMES-Pathfinder payloads, establishing their energy measurement accuracy and performance metrics.

Findings

Detectors achieved specific spectroscopic resolutions.

Energy thresholds were characterized at various temperatures.

Performance limitations of the payload architecture were identified.

Abstract

HERMES-Pathfinder is a space-borne mission based on a constellation of six nano-satellites flying in a low-Earth orbit. The 3U CubeSats, to be launched in early 2025, host miniaturized instruments with a hybrid Silicon Drift Detector/scintillator photodetector system, sensitive to both X-rays and gamma-rays. A seventh payload unit is installed onboard SpIRIT, an Australian-Italian nano-satellite developed by a consortium led by the University of Melbourne and launched in December 2023. The project aims at demonstrating the feasibility of Gamma-Ray Burst detection and localization using miniaturized instruments onboard nano-satellites. The HERMES flight model payloads were exposed to multiple well-known radioactive sources for spectroscopic calibration under controlled laboratory conditions. The analysis of the calibration data allows both to determine the detector parameters, necessary to map instrumental units to accurate energy measurements, and to assess the performance of the instruments. We report on these efforts and quantify features such as spectroscopic resolution and energy thresholds, at different temperatures and for all payloads of the constellation. Finally we review the performance of the HERMES payload as a photon counter, and discuss the strengths and the limitations of the architecture.