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This study presents numerical simulations of the touchdown process of soft landers on the lunar surface, focusing on soil footpad interaction and the resulting loading on the landing gear. Key parameters such as slope inclination, touchdown velocities, and soil properties are varied to assess their individual impacts on structural loading. The Coupled Eulerian–Lagrangian-Method (CEL) is utilized to allow for significant soil deformation during touchdown, enhancing the understanding of landing dynamics in ex

Author
puchaus1
Language
EN

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