R. Wang, G. Qiao | 2025 | Advances in Space Research
DOI 10.1016/j.asr.2025.05.050Review state
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This paper investigates the fabrication of lunar regolith fibers from the HIT-L-1 simulant, focusing on thermokinetic and rheological properties, process parameters affecting fiber diameter and temperature, and the impact of thermal post-treatment on mechanical and surface properties. The study highlights the potential of in-situ resource utilization for lunar missions. This paper presents a novel approach to the synthesis of high-performance materials from lunar regolith, with a focus on the development of fiber-reinforced composites. The study explores the feasibility of using regolith-derived materials as a sustainable alternative to traditional aerospace materials. The research includes experimental work on the processing of regolith into fibers and the evaluation of their mechanical properties. The findings suggest that the proposed method could significantly reduce the cost and environmental impact of space material production. The provided text appears to be a series of URLs and file names associated with academic or technical content, likely from a journal or publication. The URLs point to image and SVG files hosted on an AWS S3 bucket, and they are associated with specific
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Image (JPEG, PNG) and Vector Graphics (SVG)
Content Type
Academic or Technical Publication
Tensile strength
301.57 MPa
Surface energy
adjusted
Thermal treatment duration
15 min
Thermal treatment temperature
875 C
melt viscosity
negatively correlated with NBO/T
annealing temperature range
590 C to 615 C