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arXiv 2602.02461astro-ph.IMphysics.space-ph
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全 depletion p-channel Skipper-CCDs 的 X 射线表征用于 DarkNESS 任务

X-ray characterization of fully-depleted p-channel Skipper-CCDs for the DarkNESS mission

Phoenix Alpine, Ana M. Botti, Brenda A. Cervantes-Vergara, Claudio R. Chavez, Fernando Chierchie, Alex Drlica-Wagner, Juan Estrada, Erez Etzion, Michael Lembeck… 展开作者

Phoenix Alpine, Ana M. Botti, Brenda A. Cervantes-Vergara, Claudio R. Chavez, Fernando Chierchie, Alex Drlica-Wagner, Juan Estrada, Erez Etzion, Michael Lembeck, Pilar López Maggi, Joseph Noonan, Brandon Roach, Nathan Saffold, Javier Tiffenberg

AI总结:

DarkNESS 任务利用 Skipper-CCDs 在低地球轨道上探测暗物质衰变产生的 X 射线线,研究质子辐照对传感器性能的影响并评估其寿命末期的 X 射线能谱分辨率。

摘要:

Dark matter 纳卫星配备 Skipper 传感器(DarkNESS)任务是一个 6U 卫星,旨在利用 Skipper-CCDs 搜索衰变暗物质的 X 射线线。厚的、完全耗尽的 p 通道 Skipper-CCDs 提供了低读出噪声和高量子效率,适用于 1-10 keV 的 X 射线,但其在太空环境中的 X 射线性能尚未得到验证。DarkNESS 将在低地球轨道上运行,其中被束缚的质子会诱导传感器中的位移损伤,增加电荷转移效率并降低 X 射线能谱分辨率。本工作测量了 Skipper-CCDs 在质子辐照前后的 X 射线线响应,并量化了相关退化。传感器暴露于 217 MeV 质子,剂量为 8.4 x 10^10 个质子/cm²,对应位移损伤剂量超过三周年期望值的十倍。使用 55Fe 源比较了曝光四象限与相邻未曝光四象限及非辐照参考传感器的能谱分辨率。这些测量提供了 Skipper-CCDs 辐射诱导谱退化的定量评估,并使 DarkNESS 在低地球轨道上运行的寿命末期 X 射线能谱分辨率的估计成为可能。

英文摘要:

The Dark matter Nanosatellite Equipped with Skipper Sensors (DarkNESS) mission is a 6U CubeSat designed to search for X-ray lines from decaying dark matter using Skipper-CCDs. Thick, fully-depleted p-channel Skipper-CCDs provide low readout noise and high quantum efficiency for 1-10 keV X-rays, but their X-ray performance has not yet been demonstrated in the space environment. DarkNESS will operate in low-Earth orbit, where trapped protons induce displacement damage in the sensor that increases charge-transfer inefficiency and degrades the X-ray energy resolution. This work measures the X-ray line response of Skipper-CCDs before and after proton irradiation and quantifies the associated degradation. A sensor was exposed to 217 MeV protons at a fluence of 8.4 x 10^10 protons cm^-2, corresponding to a displacement-damage dose more than an order of magnitude above the three-year expectation for representative mid-inclination and Sun-synchronous low-Earth orbits. A 55Fe source was used to compare the energy resolution of the beam-exposed quadrant to adjacent unexposed quadrants and a non-irradiated reference sensor. These measurements provide a quantitative assessment of radiation-induced spectral degradation in Skipper-CCDs and enable an estimate of the end-of-life X-ray energy resolution expected for DarkNESS operation in low-Earth orbit.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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