First demonstration on direct laser fabrication of lunar regolith parts
Open accessAbstract
Purpose The purpose of this paper is to evaluate the feasibility of direct fabrication of lunar/Martian regolith simulant parts, in a freeform environment, using Laser Engineering Net Shaping (LENS™) – an additive manufacturing technology. Design/methodology/approach Bulk lunar regolith simulant structures were fabricated using a LENS™‐750. Dense parts without any macroscopic defects were produced at a laser power of 50W, a scan speed of 20 mm/s, and a powder feed rate of 12.36 g/min. The laser processed parts were characterized using X‐ray diffraction, differential scanning calorimetry, scanning electron microscope and X‐ray photoelectron spectroscopy to evaluate the influence of laser processing on the microstructure, constituent phases and chemistry of lunar regolith simulant. Findings A combination of laser parameters resulting in a 2.12 J/mm 2 laser energy appeared to be ideal for generating a melt pool necessary for lunar regolith powder deposition without excessive liquid pool spreading and cracking of solidified parts. The results show that LENS™ based laser processing transformed crystalline regolith into nanocrystalline and/or amorphous regolith structures as a result of complete melting followed by resolidification. Laser processing also resulted in marginal changes in the composition of the regolith. Originality/value Establishment of a lunar/Martian outpost necessitates the development of methods to utilize in situ mineral resources for various construction and resource extraction applications. Fabrication technologies are critical for habitat structure development, as well as repair and replacement of tools and parts at the outpost. Current experimental results presented in the paper clearly demonstrate that net shape regolith simulant parts can be fabricated using LENS™ by exploiting its capabilities.
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Balla et al. found best results with energy density 2.12 J/mm2, layer thickness 254 μm, and powder feed rate 12.35 g/min.
“The best results were obtained when using an energy density of 2 . 12 J/mm 2 while maintaining a layer thickness of 254 μm and a powder feed rate of 12.35 g/min.”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [308]
The Results and Discussion section identifies 2.12 J/mm² as an ideal laser energy, and the Methods section reports a 254 μm layer thickness for the parameter experiments. Both sections give the powder feed rate for defect-free parts as 12.36 g/min, not the claimed 12.35 g/min. Page numbers are not provided in our copy. (LLM, conf=0.90)
Experimental — accuracy not yet measuredLENS-based laser processing transformed crystalline regolith into structures with nanocrystalline and/or amorphous character, resulting from complete melting followed by solidification.
“The results indicate that LENS-based laser processing transformed crystalline regolith into structures with a nanocrystalline and/or amorphous character, resulting from complete melting followed by solidification [308].”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [308]
The Results and Discussion say laser processing appeared to transform crystalline JSC-1AC lunar regolith simulant into nanocrystalline and/or amorphous structures. They describe complete melting and resolidification as a hypothesis, whereas the citing sentence presents that mechanism as an established explanation. (LLM, conf=0.84)
Experimental — accuracy not yet measuredThis combination effectively generated the required melt pool, avoided excessive spreading of the liquid pool, and prevented cracking of solidified parts.
“This combination of parameters effectively generated the required melt pool, avoided excessive spreading of the liquid pool, and prevented the cracking of solidified parts [308].”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [308]
The material's hardness was determined to be 500 ± 18 HV.
“The material's hardness was determined to be 500 ± 18 HV.”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [308]
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References 26 · Cited by 186
Research works printed but not linked: 1
- Heiken, G. H., Vaniman, D. T., French, B. M. & Schmitt, H. H. Lunar Sourcebook. Cambridge University Press, Cambridge (1991).
- Authors
- Krishna Balla, V., Roberson, L. B., O'Connor, G. W., Trigwell, S., Bose, S., & Bandyopadhyay, A.
- Affiliations
- Kennedy Space Center (US)
- Washington State University (US)
- Venue
- Rapid Prototyping Journal
- Publisher
- Emerald
- Published
- 2012-09-28
- Volume
- 18
- Issue
- 6
- Pages
- 451-457
- ISSN
- 1355-2546 (ISSN-L)
- OpenAlex
- W1968919655
- Cited by
- 186
- References
- 26
- Citations by year
- 2026: 14 · 2025: 26 · 2024: 29 · 2023: 18 · 2022: 21 · 2021: 18 · 2020: 9 · 2019: 8 · 2018: 10 · 2017: 11 · 2016: 7 · 2015: 7 · 2014: 4 · 2013: 3 · 2012: 1
- FWCI
- 7.34
- Type
- journal article
- Language
- en
- Open access
- green
- hdl.handle.net
- Locations
- Rapid Prototyping Journal (publishedVersion)
- NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
- Funders
- W. M. Keck Foundation
- Topics
- Physical Sciences › Engineering › Mechanical Engineering › Additive Manufacturing Materials and Processes
- Physical Sciences › Engineering › Automotive Engineering › Additive Manufacturing and 3D Printing Technologies
- Physical Sciences › Engineering › Building and Construction › Innovations in Concrete and Construction Materials
- Keywords
- lunar regolith simulant, Martian regolith, direct laser fabrication, in-situ resource utilization, molten pool, nanocrystalline structure, amorphous structure, laser processing parameters, regolith composition
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