Ballistic impact testing of acrylic and alumina thin-films

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dc.contributor.author Mahalingam, Vignesh
dc.contributor.author Ranganathan, Raghavan
dc.coverage.spatial United States of America
dc.date.accessioned 2025-09-04T07:14:08Z
dc.date.available 2025-09-04T07:14:08Z
dc.date.issued 2026-01
dc.identifier.citation Mahalingam, Vignesh and Ranganathan, Raghavan, "Ballistic impact testing of acrylic and alumina thin-films", Materials Letters, DOI: 10.1016/j.matlet.2025.139351, vol. 403, Jan. 2026.
dc.identifier.issn 0167-577X
dc.identifier.issn 1873-4979
dc.identifier.uri https://doi.org/10.1016/j.matlet.2025.139351
dc.identifier.uri https://repository.iitgn.ac.in/handle/123456789/11841
dc.description.abstract High velocity projectiles cause damage to critical structures in space. Many of them travel at speeds of a few km/s to several hundred km/s. Such projectiles can punch through aircraft. In addition, bullets from modern weapons might reach 2.5 km/s. Spherical diamond projectiles are tested against Poly-Methyl-Metha-Acrylate (PMMA) and single-crystal corundum alumina (𝛼-Al2O3 ) thin films. PMMA is created from two configurations: random and oriented along impact direction. The penetration velocity (V50) of PMMA and 𝛼-alumina are found to be near 400 m/s and 4.5 km/s, respectively. This study indicates that PMMA sandwiched between two layers of alumina can be produced, with a thickness that can be calculated using specific penetration energies (𝐸∗ 𝑝 ) from the projectile radius, to stop most projectiles effectively.
dc.description.statementofresponsibility by Vignesh Mahalingam and Raghavan Ranganathan
dc.format.extent vol. 403
dc.language.iso en_US
dc.publisher Elsevier
dc.subject Molecular dynamics simulation
dc.subject Ballistic impact
dc.subject PMMA
dc.subject ?-Al2O3
dc.title Ballistic impact testing of acrylic and alumina thin-films
dc.type Article
dc.relation.journal Materials Letters


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