Article ID Journal Published Year Pages File Type
5472521 Acta Astronautica 2017 8 Pages PDF
Abstract
The experimental studies of the process of hypervelocity (up to 6 km/s) impact of a mm-size projectile on a thin aluminum plate is described. The numerical simulation of this process is presented. The data on the evolution, structure, and composition of the debris cloud formed as a result of the impact are reported. Basic specific features of the debris cloud formation are revealed.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
Authors
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