Résumé
Additive manufacturing is essential for space missions, enabling on-demand production of components where resupply from Earth is limited. Fused deposition modeling (FDM) offers a promising route for repurposing plastic packaging waste into 3D printing feedstock. Low-density polyethylene (LDPE), commonly used in space packaging, can be combined with lunar regolith simulant to increase material availability for in-situ resource utilization (ISRU). However, the method of incorporating regolith into the polymer matrix affects filament quality and printability. Here, we compare single-screw and twin-screw extrusion techniques for producing LDPE/regolith composite filaments containing up to 30 wt% regolith. Both methods successfully produced filaments suitable for FDM, though single-screw extrusion required a second extrusion step above 10 wt% regolith. Filaments were evaluated for diameter consistency and printability, including the successful fabrication of NASA-designed parts. Regolith addition enhances print performance by improving overhang formation, gap bridging, and reducing warpage. Tensile testing shows increased stiffness without compromising strength up to 20 wt% regolith. These results demonstrate that LDPE and lunar regolith can be effectively processed into printable feedstock, supporting sustainable manufacturing strategies for lunar applications and advancing terrestrial plastic waste recycling.
| langue originale | Anglais |
|---|---|
| Pages (de - à) | 409-420 |
| Nombre de pages | 12 |
| journal | Acta Astronautica |
| Volume | 237 |
| Les DOIs | |
| état | Publié - déc. 2025 |
SDG des Nations Unies
Ce résultat contribue à ou aux Objectifs de développement durable suivants
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SDG 9 – Industrie, innovation et infrastructure
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SDG 12 – Consommation et production durables
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