论文标题
对爱马仕星座和精神任务的第一个探测器飞行模型的校准
Calibration of the first detector flight models for the HERMES constellation and the SpIRIT mission
论文作者
论文摘要
爱马仕（高能卫星的高能量快速模块化集合）是一个太空传播的任务，基于在低地球轨道中飞行的六个3U立方体的星座，基于杂交硅漂移探测器/GAGG托管新的小型仪器：CE Scintiltator scintiltator potodeTector系统对X射线和X-Ray和Gamma-Rays敏感。此外，爱马仕星座将与澳大利亚 - 意大利空间行业响应智能热（Spirit）6U立方体一起运行，该稳定的热轨道（SSO）将带有一个积极冷却的爱马仕探测器探测器系统有效载荷。在本文中，我们概述了第一批爱马仕和精神飞行探测器的地面校准，概述了校准计划，探测器性能和表征。
HERMES (High Energy Rapid Modular Ensemble of Satellites) is a space-borne mission based on a constellation of six 3U CubeSats flying in a low-Earth orbit, hosting new miniaturized instruments based on a hybrid Silicon Drift Detector/GAGG:Ce scintillator photodetector system sensitive to X-rays and gamma-rays. Moreover, the HERMES constellation will operate in conjunction with the Australian-Italian Space Industry Responsive Intelligent Thermal (SpIRIT) 6U CubeSat, that will carry in a Sun-synchronous orbit (SSO) an actively cooled HERMES detector system payload. In this paper we provide an overview of the ground calibrations of the first HERMES and SpIRIT flight detectors, outlining the calibration plan, detector performance and characterization.
