Y. Yang, M. Rahman, M. Andriamasinoro, F. Vatteroni, L. Wang | 2026 | Acta Astronautica
DOI 10.1016/j.actaastro.2026.04.066Review state
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This study compares the morphological and mechanical properties of lunar regolith simulants LHS-1, LMS-1, and LSP-2 using micro-CT reconstruction and direct shear tests. The results show differences in shear strength and internal friction angles, with LSP-2 having the highest internal friction angle. The provided text is a mix of metadata, references, and possibly parts of a research paper or article. It includes information about the paper's title, authors, journal, publication date, and other technical details. There are also references to other works and authors, which may be citations or related studies. The text also contains links to images and files associated with the paper, such as PDFs and JPEGs. The main content of the paper seems to focus on lunar regolith simulants, particle size analysis, and possibly their applications in space exploration or extreme environments. The provided text appears to be a series of URLs and file names associated with images or documents, likely from an academic or technical paper. The URLs are structured with a common base URL (`https://s3-eu-west-1.amazonaws.com/prod-ucs-content-store-eu-west/`) and include paths to content related to speci
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Particle size analysis
Physical property measurement
Mechanical behavior under stress
Material testing
CT Image Segmentation
Imaging
3D Curvature Analysis
Imaging
Direct Shear Testing
Mechanical Testing
Principal Component Analysis (PCA)
Data Analysis
micro-CT reconstruction
morphological
direct shear tests
mechanical
Particle size distribution
1 mm
Simulant type
Lunar regolith
Application
Space exploration
Identifier
S0094576526003000
Internal Friction Angle
Semi-quantitative relationship with mechanical properties
Morphological Discrimination
Based on standardized three-dimensional shape descriptors
Shear Stress-Normal Stress Relationship
Fitted Mohr-Coulomb envelopes
D10 (mm)
0.0417