Compact potential sensor for spacecraft based on a silicon photonic waveguide

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Authors: Kosei Otsuka, Wataru Takahama, Takeki Higashiguchi, Kazuya Kikunaga, Rikuto Hojo, Tomofumi Mogami, Kazuhiro Toyoda, Yasushi Takahashi
Cited by: 1
References: 47

Abstract

Abstract Satellites charge up due to incoming electrons and ions, resulting in an electrical potential difference (Δ V ) between the satellite and outer space. This can cause electrostatic discharge (ESD) events, damaging electronic devices. To reduce failures due to ESD, sensors monitoring the Δ V can be helpful. Due to spacecraft’s restrictions, the sensors should be as small as possible. While small potential sensors in terrestrial applications are often based on electrical conduction in semiconductors, such sensors are not suitable for space application due to a weak resistance to cosmic radiation and ESD. Here, we report a compact sensor based on another sensing method: the utilization of light absorption in a silicon photonic waveguide. We performed experiments in a vacuum chamber simulating the space plasma environment to demonstrate that the light attenuation in the waveguide is depends on the Δ V . Our results further indicate that our sensor exhibits a high resistance to ESD.

Fields of Study & Subjects

Ionosphere and magnetosphere dynamics Space Satellite Systems and Control Geophysics and Sensor Technology

Publication details

Journal / source
Research Square
Publisher
Springer Science and Business Media LLC
Volume
3
Issue
1
Pages
10
Publication date
13 January 2026
Language
EN
Document type
Preprint