Numerical Analysis of Coaxially 3D Printed Lunar Habitats: Integrating Regolith and PCM for Passive Temperature Control

Abstract Space research is shifting its focus from low-gravity platforms to Moon and Mars exploration, requiring advanced habitat construction. This paper proposes to integrate the 3D printing of regolith and Phase Change Materials (PCM), with a particular interest in lunar habitats. A coaxial printing approach is numerically analyzed, enabling the simultaneous deposition of a regolith shell, providing structural integrity, and a PCM core that helps regulate the interior habitat temperature in a passive manner. Simulations show that 3D printing with a coaxial nozzle can effectively control the shell-core (internal) structure of the habitat wall by adjusting printing parameters or by constructing multi-strand composite walls. The PCM core becomes thicker when using a smaller layer height or a higher extrusion speed during printing. We then examine the expected thermal response of the habitat, initially made of pure regolith and later incorporating the PCM. With just regolith, results indicate that one can select adequate thermo-optical properties at the wall external boundary, and wall thickness, to control the mean temperature in the interior, and associated fluctuations, respectively. Incorporating the PCM, either in single or multiple regolith-PCM strands, is shown to effectively stabilize this internal temperature ( $$\Delta T_\textrm{i} \rightarrow 0$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:mi>Δ</mml:mi> <mml:msub> <mml:mi>T</mml:mi> <mml:mtext>i</mml:mtext> </mml:msub> <mml:mo>→</mml:mo> <mml:mn>0</mml:mn> </mml:mrow> </mml:math> K), improving thermal performance and habitat design, and reducing the quantity of required regolith and binder. Since binder has to be brought from Earth, this reduction can be a major factor in enabling sustainable construction on the Moon and beyond.

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Publication Details

Journal
Microgravity Science and Technology
Published
2025-07-05
DOI
https://doi.org/10.1007/s12217-025-10194-4
Citations
3
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
14.98

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article

Numerical Analysis of Coaxially 3D Printed Lunar Habitats: Integrating Regolith and PCM for Passive Temperature Control

Md. Tusher Mollah, J.M. Ezquerro, P. Sánchez, Jon Spangenberg et al.
3 citations
Microgravity Science and Technology
Spacecraft and Cryogenic Technologies
14.98
article

Numerical Analysis of Coaxially 3D Printed Lunar Habitats: Integrating Regolith and PCM for Passive Temperature Control

Md. Tusher Mollah, J.M. Ezquerro, P. Sánchez, Jon Spangenberg, Berin Šeta, A. Borshchak Kachalov
article en
3 citations

Abstract

Abstract Space research is shifting its focus from low-gravity platforms to Moon and Mars exploration, requiring advanced habitat construction. This paper proposes to integrate the 3D printing of regolith and Phase Change Materials (PCM), with a particular interest in lunar habitats. A coaxial printing approach is numerically analyzed, enabling the simultaneous deposition of a regolith shell, providing structural integrity, and a PCM core that helps regulate the interior habitat temperature in a passive manner. Simulations show that 3D printing with a coaxial nozzle can effectively control the shell-core (internal) structure of the habitat wall by adjusting printing parameters or by constructing multi-strand composite walls. The PCM core becomes thicker when using a smaller layer height or a higher extrusion speed during printing. We then examine the expected thermal response of the habitat, initially made of pure regolith and later incorporating the PCM. With just regolith, results indicate that one can select adequate thermo-optical properties at the wall external boundary, and wall thickness, to control the mean temperature in the interior, and associated fluctuations, respectively. Incorporating the PCM, either in single or multiple regolith-PCM strands, is shown to effectively stabilize this internal temperature ( $$\Delta T_\textrm{i} \rightarrow 0$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"> <mml:mrow> <mml:mi>Δ</mml:mi> <mml:msub> <mml:mi>T</mml:mi> <mml:mtext>i</mml:mtext> </mml:msub> <mml:mo>→</mml:mo> <mml:mn>0</mml:mn> </mml:mrow> </mml:math> K), improving thermal performance and habitat design, and reducing the quantity of required regolith and binder. Since binder has to be brought from Earth, this reduction can be a major factor in enabling sustainable construction on the Moon and beyond.

Microgravity Science and TechnologyVol. 37(4)
Universidad Politécnica de Madrid (ES), Technical University of Denmark (DK)
Innovationsfonden, Ministerio de Ciencia, Innovación y Universidades, Ministerio de Ciencia e Innovación, Danmarks Tekniske Universitet
Openalex Percentile: Top 2%
Spacecraft and Cryogenic Technologies
14.98
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