Evaluation of ALON for Proton Shielding of Low Earth Orbit (LEO) Satellite Solar Arrays

C. Firat

Abstract


This study evaluates the proton radiation shielding efficacy of various materials, with a focus on ALON, for satellite solar arrays in LEO across the 0.1-200 MeV energy range using SRIM/TRIM simulations. Key metrics, ion penetration, vacancies per ion, range, displacements per atom, non-ionizing energy loss, Bragg curves, and transmission, were analyzed for aluminum, SiO2, polyimide, ALON, and Ta2O5/Al2O3 at thicknesses from 0.01 mm to 4 mm. ALON demonstrates moderate stopping power and damage resistance, with penetration exceeding 20 µm and 100 µm at 0.5 MeV and 5 MeV, respectively, and 2000 µm and 4000 µm providing protection up to 50 MeV and 100 MeV, while maintaining high optical clarity (>80%) for photovoltaic (PV) applications. Thinner layers mitigate high-energy proton damage but are vulnerable to low-energy (<1 MeV) peaks in DPA and NIEL, whereas thicker layers offer broader shielding at the cost of increased damage accumulation. Multi-criteria decision analysis highlights ALON’s suitability for LEO, balancing mass, radiation protection, and optical functionality. These findings, validated with 5% agreement with literature, suggest ALON as a promising PV shield, with future research needed to address high-energy protons and secondary particle effects.

Keywords


Proton Radiation Shielding, Aluminum Oxynitride (ALON), Satellite Solar Arrays, SRIM/TRIM Simulations, Satellite Orbits

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DOI: https://doi.org/10.55981/aij.2026.1724



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