Proton-Radiation-Tolerant Silicon Photonic Charge Sensor for Spacecraft Applications

IF 5
Wataru Takahama, Kosei Otsuka, Ayumi Ishihara, Rikuto Hojo, Tomofumi Mogami, Kazuhiro Toyoda, Kohtaku Suzuki, Yasushi Takahashi
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Abstract

Silicon waveguides are promising platforms for spacecraft potential sensing owing to their compactness and immunity to electromagnetic interference. However, proton-induced optical absorption in operating silicon waveguides has not been quantitatively clarified, despite their direct exposure to the space radiation environment during spacecraft operation. Here, we present a systematic elucidation of proton-radiation effects on a photonic charge sensor based on silicon photonic crystal waveguides. During proton irradiation at 20 keV, we quantitatively evaluate the increase in optical absorption under device operation and find that a fluence of 1.0 × 1014 cm−2 induces an additional absorption coefficient of approximately 0.41 cm−1. We further demonstrate that the sensor retains its ability to measure spacecraft potential even after exposure to a high proton fluence of 1.0 × 1015 cm−2, confirming its intrinsic radiation tolerance. These results establish the radiation robustness of silicon-waveguide-based sensing mechanisms and provide the first quantitative basis for implementing photonic charge sensors in radiation-rich spacecraft environments.

用于航天器的耐质子辐射硅光子电荷传感器
硅波导结构紧凑,抗电磁干扰能力强,是航天器电位传感的理想平台。然而,尽管硅波导在航天器运行过程中直接暴露在空间辐射环境中,但其在运行过程中质子诱导的光吸收尚未得到定量澄清。本文系统地阐述了基于硅光子晶体波导的光子电荷传感器的质子辐射效应。在20 keV的质子辐照下,我们定量地评估了器件操作下光吸收的增加,发现1.0 × 1014 cm−2的影响诱导了大约0.41 cm−1的额外吸收系数。我们进一步证明,即使暴露在1.0 × 1015 cm−2的高质子通量下,传感器仍保持测量航天器电位的能力,证实了其固有的辐射耐受能力。这些结果建立了基于硅波导的传感机制的辐射鲁棒性,并为在辐射丰富的航天器环境中实现光子电荷传感器提供了第一个定量依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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