Low binder content bricks: a regolith-based solution for sustainable surface construction on the Moon

被引:4
作者
Torre, Roberto [1 ]
Cowley, Aidan [1 ]
Ferro, Carlo Giovanni [2 ]
机构
[1] European Astronaut Ctr, ESA, Cologne, Germany
[2] Politecn Torino, Dept Mech & Aerosp Engn, Turin, Italy
关键词
ISRU; Lunar regolith; Thermoplastic; Moon; Concrete; Bricks; MECHANICAL-PROPERTIES; LUNAR; CEMENT;
D O I
10.1007/s42452-024-05717-4
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
This work proposes a composite construction material made by a blend of lunar regolith and thermoplastic binders in dry powder form. This solution offers advantages over regolith sintering or melting by requiring lower power consumption and simplifying the manufacturing process. However, its sustainability depends on minimizing the content of the binder material. Drawing from validated concepts used on Earth, such as polymeric concrete and compressed Earth bricks, this paper suggests that binder optimization can be achieved by simplifying and streamlining the manufacturing process, targeting parts with predefined shapes. Standardized elements like bricks or tiles ease production and assembly automation, especially when incorporating interlocking features, simplifying the payload concept transition. After drafting the process with a minimum number of basic steps, this work studies the effects of some process parameters to minimize the weight percentage of the matrix while maintaining reasonable mechanical properties. The compressive and the flexural strength are the targets of an orthogonal array Design of Experiment. Through comparison with reference values for civil engineering, the process demonstrates promising results within an organic phase as low as 10 wt%. A manufacturing process easily scalable to larger-sized products is proposed for a regolith-rich composite material. Adjusting the binder weight percentage, compaction pressure, and regolith grain size improves the mechanical properties. A minimal binder allows for reaching possible compression and flexural strength requirements for lunar construction.
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页数:15
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