Radiation‐Resistant Aluminum Alloy for Space Missions in the Extreme Environment of the Solar System

P Patrick D. Willenshofer (Chair of Non‐Ferrous Metallurgy Deparment Metallurgy Montanuniversität Leoben Franz‐Josef‐Straße 18 8700 Leoben Austria) M Matheus A. Tunes H Hi T. Vo L Lukas Stemper (AMAG rolling GmbH Lamprechtshausener Str. 61 5282 Ranshofen Austria) M Markus Alfreider (Department of Materials Science) O Oliver Renk G Graeme Greaves (United Kingdom Atomic Energy Authority Culham Campus OX14 3DB Abingdon UK) D Daniel Kiener P Peter J. Uggowitzer (Chair of Non‐Ferrous Metallurgy Deparment Metallurgy Montanuniversität Leoben Franz‐Josef‐Straße 18 8700 Leoben Austria) S Stefan Pogatscher

Abstract

Abstract Future human exploration of the solar system demands advanced materials capable of withstanding extreme environments, particularly exposure to solar energetic particle radiation. Current material selection criteria for space applications prioritize a high strength‐to‐weight ratio, high corrosion resistance and manufacturability, favoring age‐hardenable Al‐based alloys. However, conventional precipitation‐hardened Al alloys suffer from irradiation‐assisted dissolution of strengthening phases at doses as low as 0.2 displacements‐per‐atom (dpa), undermining their performance. Furthermore, these alloys develop radiation‐induced defects, such as dislocation loops and voids, even at low doses. This study presents a novel ultrafine‐grained (UFG) Al‐based alloy, designed using the crossover alloying concept and strengthened by T‐phase precipitates, featuring a chemically‐complex structure with 162 atoms in its unit cell composed of Mg 32 (Zn,Al) 49 . It is showed that T‐phase precipitates have exceptional radiation tolerance up to 24 dpa. Owing to the nanoscale UFG structure, dislocation loops are suppressed, and voids are only observed beyond 75 dpa. Microtensile tests up to 20 dpa confirm the preservation of mechanical performance under irradiation. The results underline the potential of this alloy as a radiation‐resistant, lightweight material for future space applications. Three key strategies enable this performance: (i) stabilization of a UFG microstructure, (ii) T‐phase precipitation featuring a highly negative Gibbs free energy and chemically‐complex giant unit cell, and (iii) precise process control to prevent grain growth during heat treatment and irradiation.

Article Details

Volume / Issue Vol. 38, Issue 20
Published April 01, 2026
ISSN 0935-9648
Publisher Unknown Publisher

Journal Info

Advanced Materials

Unknown Publisher

ISSN: 0935-9648 Physical Sciences

Authors (10)

P

Patrick D. Willenshofer

Chair of Non‐Ferrous Metallurgy Deparment Metallurgy Montanuniversität Leoben Franz‐Josef‐Straße 18 8700 Leoben Austria

M

Matheus A. Tunes

H

Hi T. Vo

L

Lukas Stemper

AMAG rolling GmbH Lamprechtshausener Str. 61 5282 Ranshofen Austria

M

Markus Alfreider

Department of Materials Science

O

Oliver Renk

G

Graeme Greaves

United Kingdom Atomic Energy Authority Culham Campus OX14 3DB Abingdon UK

D

Daniel Kiener

P

Peter J. Uggowitzer

Chair of Non‐Ferrous Metallurgy Deparment Metallurgy Montanuniversität Leoben Franz‐Josef‐Straße 18 8700 Leoben Austria

S

Stefan Pogatscher