用于 NewAthena X-IFU 的时分复用读出的低温试验台的系统性能

Davide Vaccaro, Jan van der Kuur, Paul van der Hulst, Tobias Vos, Martin de Wit, Luciano Gottardi, Kevin Ravensberg, Emanuele Taralli, Joseph Adams, Simon Bandler, Douglas Bennet, James Chervenak, Bertrand Doriese, Malcolm Durkin, Jonathan Gard, Carl Reintsema, Kazuhiro Sakai, Steven Smith, Joel Ullom, Nicholas Wakeham, Jan-Willem den Herder, Brian jackson, Pourya Khosropanah, Jian-Rong Gao, Peter Roelfsema, Aurora Simionescu
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摘要

X射线积分场单元(X-IFU)是欧空局未来新雅典娜空间观测站的一个仪器,目标是通过一个由大约1500个过渡边传感器(TES)组成的阵列,通过SQUID时分复用(TDM)读出,在200eV到12keV的X射线能量范围内提供高能量分辨率(在X射线能量达到7keV时小于4eV)和高空间分辨率(9")光谱成像。2022 年,为了帮助 TDM 读出技术从实验室向飞行硬件转移,我们的团队在 SRON 调试了一个新的基于 TDM 的实验室测试平台。这个装置承载了75次75\mu$m$^2$ TES阵列,通过2列32行TDM读出。对高性能运行至关重要的系统组件是连接室温电子元件和致冷读出元件的线束。2023 年 11 月,我们采用了重新设计的柔性线束,在 SRON 试验台中,该线束的长度接近 X-IFU 飞行线束的预期长度。我们在此报告使用新柔性线束的TDM系统的特性,该系统通过32行读出,在6~keV时达到了2.7~eV FWHM的共加能量分辨率。此外,我们还对即将把 TDM 读出集成到 X-IFU 焦平面组件开发模型中进行了展望。
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System performance of a cryogenic test-bed for the time-division multiplexing readout for NewAthena X-IFU
The X-ray Integral Field Unit (X-IFU) is an instrument of ESA's future NewAthena space observatory, with the goal to provide high-energy resolution ($<$ 4 eV at X-ray energies up to 7 keV) and high-spatial resolution (9") spectroscopic imaging over the X-ray energy range from 200 eV to 12 keV, by means of an array of about 1500 transition-edge sensors (TES) read out via SQUID time-division multiplexing (TDM). In 2022, to aid in the transfer of TDM readout technology from the laboratory toward flight hardware, our team commissioned a new TDM-based laboratory test-bed at SRON. This setup hosts an array of $75\times 75\ \mu$m$^2$ TESs that are read out via 2-column $\times$ 32-row TDM. A system component that is critical to high-performance operation is the wiring harness that connects the room-temperature electronics to the cryogenic readout componentry. In November 2023, we implemented a re-designed flex harness, which in the SRON test-bed has a length close to what is envisioned for the X-IFU flight harness. We report here on our characterization of the TDM system with the new flex harness, which allowed the system to achieve a co-added energy resolution at a level of 2.7~eV FWHM at 6~keV via 32-row readout. In addition, we provide an outlook on the upcoming integration of TDM readout into the X-IFU Focal-Plane Assembly Development Model.
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