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Orbit-Coupled Multiphysics Degradation Modelling of CubeSat Lithium-Ion Batteries

CubeSats operate under severe orbital thermal cycling and limited thermal control authority, making lithium-ion battery degradation a primary mission-limiting factor. Repeated sunlight–eclipse transitions in low Earth orbit induce high-frequency temperature oscillations, while progressive internal r...

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Bibliografiske detaljer
Hovedforfatter: Aswin KARKADAKATTIL
Format: Artigo
Sprog:Inglês
Udgivet: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2026-03-01
Serier:INCAS Bulletin
Fag:
Online adgang:https://bulletin.incas.ro/files/karkadakattil-a_vol_18_iss_1.pdf
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