Additive Manufacturing of PEEK/Lunar Regolith Composites for Sustainable Lunar Manufacturing

TL;DR

This study explores 3D printing PEEK composites with lunar regolith simulant for sustainable lunar construction, analyzing how regolith content affects material properties and processability.

Contribution

It introduces a method for additive manufacturing of lunar regolith-PEEK composites, detailing processing parameters and property trade-offs for in-situ lunar resource utilization.

Findings

Densities above 96% achieved in all filaments.

Increased regolith content enhances crystallinity and elastic modulus.

Tensile strength decreases with higher regolith loading, especially beyond 40 wt%.

Abstract

As humanity advances toward long-term lunar presence under NASA's Artemis program, the development of lunar-based manufacturing and construction (LBMC) capabilities has become increasingly critical. The high cost of transporting materials from Earth makes in-situ resource utilization (ISRU) essential, with lunar regolith serving as a promising local feedstock. Additive manufacturing (AM) offers a compelling platform for LBMC due to its geometric flexibility, material efficiency, and capacity for on-demand, site-specific production. This study investigates material extrusion (MEX) AM of polyether-ether-ketone (PEEK) composites containing 10 to 50 wt% lunar regolith simulant (LRS). PEEK and LMS-1D powders were melt-compounded via twin-screw extrusion, printed using a high-temperature chamber, and annealed at 300 degrees C. The samples were characterized through density measurements, thermal analysis, tensile testing, and microstructural and elemental mapping. All filaments exhibited densities above 96%, though as-printed porosity increased from less than 1% in neat PEEK to 7.5% at 50 wt% LRS due to elevated melt viscosity. Regolith incorporation enhanced crystallinity (17.4 to 20.5%) and elastic modulus (by 6-41%), while reducing delamination and warping, which improved dimensional accuracy and print success rates. Tensile strength declined gradually from 107 MPa to 90 MPa up to 40 wt% LRS, then dropped sharply to approximately 70 MPa at 50 wt%. Annealing improved density and stiffness for composites containing up to 30 wt% LRS, with marginal benefit at higher contents. Microstructural and elemental analyses confirmed a continuous PEEK matrix with uniformly dispersed regolith particles. This work establishes processing windows and trade-offs for regolith-rich PEEK composites, supporting ISRU-enabled AM of future lunar infrastructure.