Satellite Internal Charging for a Reasonable Worst‐Case
Horne, R.B. ORCID: https://orcid.org/0000-0002-0412-6407; Lam, P.Y.; Meredith, N.P.
ORCID: https://orcid.org/0000-0001-5032-3463; Glauert, S.A.
ORCID: https://orcid.org/0000-0003-0149-8608; Kirsch, P.
ORCID: https://orcid.org/0000-0003-2482-0217.
2025
Satellite Internal Charging for a Reasonable Worst‐Case.
Space Weather, 23 (6), e2024SW004226.
15, pp.
10.1029/2024SW004226
Preview |
Text (Open Access)
© 2025. The Author(s). Space Weather - 2025 - Horne - Satellite Internal Charging for a Reasonable Worst‐Case.pdf - Published Version Available under License Creative Commons Attribution 4.0. Download (3MB) | Preview |
Abstract/Summary
Increases in the flux of high energy electrons in the Earth's radiation belts cause satellite charging which can lead to an electrostatic discharge, anomalies and disruption to service. For geostationary orbit (GEO) there are guidelines on how much shielding to protect electronic components, but not for lower orbits. Here we use data from GPS satellite NS41, the AE9 radiation model, and LANL satellite data to create a reasonable worst-case electron flux spectrum between 60 keV and 8 MeV. We calculate the charging currents for satellites in circular equatorial orbit between 4.25 and 7.0 Re and show that the recommended guideline of 2.8 mm (110 mil) of Al shielding is sufficient to keep charging below recommended guidelines at GEO. Approximately 4.5 mm (177 mil) of Al shielding would be needed for satellites in circular equatorial orbit at 4.5 Re. We show that the maximum electric field could exceed the breakdown field in cables and dielectrics just under the spacecraft surface on a timescale of 1–2 hr presenting a risk of anomalies. Radiation induced conductivity reduces the risk but is highly uncertain. A magnetic storm, series of storms or high speed stream accompanied by a large solar energetic particle event would present a much higher risk of anomalies on several satellites.
Item Type: | Publication - Article |
---|---|
Digital Object Identifier (DOI): | 10.1029/2024SW004226 |
ISSN: | 1542-7390 |
Additional Keywords: | satellite charging, internal charging, severe space weather, surface charging, reasonable worst case |
Date made live: | 16 Jun 2025 08:43 +0 (UTC) |
URI: | https://nora.nerc.ac.uk/id/eprint/539595 |
Actions (login required)
![]() |
View Item |
Document Downloads
Downloads for past 30 days
Downloads per month over past year