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硬X射线立方星偏振仪的在轨背景:低地轨道CUSP任务案例研究

In orbit background for hard X-ray CubeSat polarimeters: case study of the CUSP mission in low-earth orbit

Abhay Kumar, Giovanni Lombardi, Riccardo Campana, Giovanni De Cesare, Sergio Fabiani, Ettore Del Monte, Andrea Alimenti, Enrico Costa, Mauro Centrone, Nicolas De Angelis, Sergio Di Cosimo, Giuseppe Di Persio, Pasqualino Loffredo, Gabriele Minervini, Fabio Muleri, Paolo Romano, Alda Rubini, Emanuele Scalise, Enrico Silva, Paolo Soffitta, Giovanni Cucinella, Vito Di Bari, Simone Di Filippo, Andrea Negri, Massimo Perelli, Dario Modenini, Andrea Curatolo, Nicolas Gagliardi, Daniele Pecorella, Alice Ponti, Paolo Tortora, Andrea Del Re, Davide Albanesi, Valerio Campamaggiore, Giulia de Iulis, Adam Ebrahim, Paolo Leonetti, Marco Schepis, Alessandro Zambardi, Ilaria Baffo, Pierluigi Fanelli, Costantino Zazza, Valerio Vagelli, Daniele Brienza, Immacolata Donnarumma, Matteo Merge, Emanuele Zaccagnino, Alessandro Turchi

arXiv 2608.01524首次发表:更新:

AI 中文总结

该研究针对低地轨道CUSP任务,利用Geant4模拟器结合详细质量模型,估算硬X射线立方星偏振仪的在轨背景,以优化探测器几何与屏蔽,提升信噪比性能。

AI 中文摘要

立方星太阳偏振仪(CUSP)项目旨在利用康普顿散射偏振仪测量25-100 keV硬X射线波段太阳耀斑的线性偏振,该项目属于意大利空间局Alcor计划框架,用于开发创新立方星技术与任务。作为CUSP于2024年12月启动、2026年7月2日结束的B阶段研究的一部分,估算在轨背景以优化信噪比是关键目标之一。在低地轨道,该仪器暴露于宇宙与反照X射线背景、带电粒子以及航天器和大气产生的次级辐射中,模拟这些贡献可优化探测器几何结构与屏蔽,以最大化信噪比性能。我们使用基于Geant4的模拟器给出CUSP的初始在轨背景估算,已构建CUSP的详细质量模型,用于模拟背景分量并估算CUSP轨道的背景计数率。

英文摘要

The CUbesat Solar Polarimeter (CUSP) project aims to measure the linear polarization of solar flares in the 25 - 100 keV hard X-ray band using a Compton scattering polarimeter. CUSP is a project in the framework of the Alcor Program of the Italian Space Agency aimed to develop innovative CubeSat technologies and missions. As part of CUSPs Phase B study, initiated in December 2024 and closed on July 2nd, 2026, estimating the in orbit background to optimize the signal-to-background ratio was one of the key objectives. In low-Earth orbit, the instrument is exposed to cosmic and albedo X-ray backgrounds, charged particles, and secondary radiation from the spacecraft and atmosphere. Simulating these contributions enables optimization of detector geometry and shielding to maximize signal-to-noise performance. We present initial in orbit background estimates for CUSP using a Geant4-based simulator. A detailed mass model of the CUSP has been implemented to simulate background components and estimate the background count rate in the CUSP orbit.

Comments8 pages, 4 figures, Submitted to SPIE Astronomical Telescopes + Instrumentation, Comments are welcome!

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