Compact potential sensor for spacecraft based on a silicon photonic waveguide
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 depends on the Δ V . Our results further indicate that our sensor exhibits a high resistance to ESD.
Authors
- Kazuya Kikunaga (ORCID: https://orcid.org/0000-0002-1398-3080)
- Rikuto Hojo
- Takeki Higashiguchi
- Wataru Takahama
- Tomofumi Mogami
- Yasushi Takahashi
- Kazuhiro Toyoda
- Kosei Otsuka
Institutions
- Okayama University (JP)
- Kyushu Institute of Technology (JP)
- Denka (Japan) (JP)
- Osaka Metropolitan University (JP)
- Tokyo Metropolitan University (JP)
- National Institute of Advanced Industrial Science and Technology (JP)
Publication Details
- Journal
- npj Nanophotonics
- Published
- 2026-02-02
- DOI
- https://doi.org/10.1038/s44310-025-00100-6
- Primary Topic
- Ionosphere and magnetosphere dynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- Japan Society for the Promotion of Science