S. Moazen, F. Gosselin, I. Tabiai, M. Dubé | 2025 | Acta Astronautica
DOI 10.1016/j.actaastro.2025.08.012Review state
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This paper explores the 3D printing of LDPE/lunar regolith simulant composites for in-situ resource utilization on the Moon. It compares single-screw and twin-screw extrusion methods for producing filaments with up to 30 wt% regolith. The study evaluates printability, tensile properties, and filament consistency, demonstrating the feasibility of using lunar regolith simulants in sustainable manufacturing for lunar applications. This study explores the use of Lunar mare regolith simulant (LMS-1D) for FFF 3D printing applications. LMS-1D, a commercially available mineral-based material, is designed to replicate the average composition of mare-type lunar soil. It has a particle size range of 0.04–35 µm, with a mean size of 6 µm. This size distribution was selected over one that more closely resembles Apollo regolith, as it is better suited for FFF 3D printing and can be used as received, eliminating the need for additional milling, which is typically required to avoid nozzle clogging when larger particles are present. An SEM image of the particles is shown in Fig. S1 (see Supporting Document). The paper discusses the fabrication of filaments using three different extrusion processes:
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Single-screw extrusion
Material processing | 3D printing feedstock production
Material processing optimization
Material processing | 3D printing feedstock production
SEM imaging of LMS-1D particles
visualization
Comparison with JSC-1 simulant and Apollo regolith
comparison
SS1
One-pass single screw extruder
SS2
Twice-extruded single screw extruder
TS1
One-pass twin screw extruder
Single-screw extrusion
filament production
Comparison material
JSC-1 simulant and Apollo regolith
Visualization
SEM image
Funding organization
CREPEC
Outgassing
occurs in vacuum conditions
Melt flow index
0.9 g/10 min (190/2.16)
Density
0.922 g/cm3
Melt flow index
8 g/10 min (190/2.16)
Density
0.918 g/cm3