Y. Jiang, F. Li, S. Zhou, L. Liu | 2025 | Case Studies in Construction Materials
DOI 10.1016/j.cscm.2024.e04132Review state
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This paper investigates the vacuum-sintered BH-1 lunar regolith simulant for lunar in-situ construction. It evaluates microstructural, mechanical, and thermal properties using XRD, SEM, nanoindentation, uniaxial compression, and thermal property tests. The sintering temperature significantly affects microstructure and mechanical strength, with a maximum compressive strength of 90 MPa at 1100 C. The BH-1 LRS exhibits a low coefficient of thermal expansion (CTE) within 150 C to 150 C. The paper discusses the investigation of the Chang'e-5 lunar samples and their potential applications in lunar construction. It highlights the production properties of regolith polymer composites for lunar construction, emphasizing the importance of material selection for sustainable lunar habitats. The study also references previous research on lunar regolith and its use in construction materials. The provided text contains a series of URLs and file names related to images and thumbnails, likely from a scientific or academic paper. The URLs are associated with different image sizes (thumbnail, high-resolution) and are hosted on an AWS S3 bucket. The file names include identifiers like 'gr1', 'gr2', etc
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XRD
X-ray diffraction
SEM
Scanning electron microscopy
Nanoindentation
Nanoindentation
Uniaxial compression
Uniaxial compression
Thermal property tests
Thermal property tests
Sintering at Various Temperatures
Thermal Processing
Thermal Characterization
Material Analysis
Microstructural Analysis
Material Characterization
Thermal Properties
Characterized in Fig. 1
Microstructure
Analyzed via SEM and MIP
Mechanical Properties
Measured via Nanoindentation
Phase Composition
Analyzed via XRD
compressive strength
90 MPa
coefficient of thermal expansion (CTE)
low
microstructure
affected by sintering temperature
mineral composition
unchanged at different sintering temperatures