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Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks
Here, we present a comprehensive approach for creating robust, elastic, designer Lunar and Martian regolith simulant (LRS and MRS, respectively) architectures using ambient condition, extrusion-based 3D-printing of regolith simulant inks. The LRS and MRS powders are characterized by distinct, highly...
Autores principales: | , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Nature Publishing Group
2017
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5357966/ https://www.ncbi.nlm.nih.gov/pubmed/28317904 http://dx.doi.org/10.1038/srep44931 |
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author | Jakus, Adam E. Koube, Katie D. Geisendorfer, Nicholas R. Shah, Ramille N. |
author_facet | Jakus, Adam E. Koube, Katie D. Geisendorfer, Nicholas R. Shah, Ramille N. |
author_sort | Jakus, Adam E. |
collection | PubMed |
description | Here, we present a comprehensive approach for creating robust, elastic, designer Lunar and Martian regolith simulant (LRS and MRS, respectively) architectures using ambient condition, extrusion-based 3D-printing of regolith simulant inks. The LRS and MRS powders are characterized by distinct, highly inhomogeneous morphologies and sizes, where LRS powder particles are highly irregular and jagged and MRS powder particles are rough, but primarily rounded. The inks are synthesized via simple mixing of evaporant, surfactant, and plasticizer solvents, polylactic-co-glycolic acid (30% by solids volume), and regolith simulant powders (70% by solids volume). Both LRS and MRS inks exhibit similar rheological and 3D-printing characteristics, and can be 3D-printed at linear deposition rates of 1–150 mm/s using 300 μm to 1.4 cm-diameter nozzles. The resulting LRS and MRS 3D-printed materials exhibit similar, but distinct internal and external microstructures and material porosity (~20–40%). These microstructures contribute to the rubber-like quasi-static and cyclic mechanical properties of both materials, with young’s moduli ranging from 1.8 to 13.2 MPa and extension to failure exceeding 250% over a range of strain rates (10(–1)−10(2) min(−1)). Finally, we discuss the potential for LRS and MRS ink components to be reclaimed and recycled, as well as be synthesized in resource-limited, extraterrestrial environments. |
format | Online Article Text |
id | pubmed-5357966 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2017 |
publisher | Nature Publishing Group |
record_format | MEDLINE/PubMed |
spelling | pubmed-53579662017-03-22 Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks Jakus, Adam E. Koube, Katie D. Geisendorfer, Nicholas R. Shah, Ramille N. Sci Rep Article Here, we present a comprehensive approach for creating robust, elastic, designer Lunar and Martian regolith simulant (LRS and MRS, respectively) architectures using ambient condition, extrusion-based 3D-printing of regolith simulant inks. The LRS and MRS powders are characterized by distinct, highly inhomogeneous morphologies and sizes, where LRS powder particles are highly irregular and jagged and MRS powder particles are rough, but primarily rounded. The inks are synthesized via simple mixing of evaporant, surfactant, and plasticizer solvents, polylactic-co-glycolic acid (30% by solids volume), and regolith simulant powders (70% by solids volume). Both LRS and MRS inks exhibit similar rheological and 3D-printing characteristics, and can be 3D-printed at linear deposition rates of 1–150 mm/s using 300 μm to 1.4 cm-diameter nozzles. The resulting LRS and MRS 3D-printed materials exhibit similar, but distinct internal and external microstructures and material porosity (~20–40%). These microstructures contribute to the rubber-like quasi-static and cyclic mechanical properties of both materials, with young’s moduli ranging from 1.8 to 13.2 MPa and extension to failure exceeding 250% over a range of strain rates (10(–1)−10(2) min(−1)). Finally, we discuss the potential for LRS and MRS ink components to be reclaimed and recycled, as well as be synthesized in resource-limited, extraterrestrial environments. Nature Publishing Group 2017-03-20 /pmc/articles/PMC5357966/ /pubmed/28317904 http://dx.doi.org/10.1038/srep44931 Text en Copyright © 2017, The Author(s) http://creativecommons.org/licenses/by/4.0/ This work is licensed under a Creative Commons Attribution 4.0 International License. The images or other third party material in this article are included in the article’s Creative Commons license, unless indicated otherwise in the credit line; if the material is not included under the Creative Commons license, users will need to obtain permission from the license holder to reproduce the material. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/ |
spellingShingle | Article Jakus, Adam E. Koube, Katie D. Geisendorfer, Nicholas R. Shah, Ramille N. Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title | Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title_full | Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title_fullStr | Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title_full_unstemmed | Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title_short | Robust and Elastic Lunar and Martian Structures from 3D-Printed Regolith Inks |
title_sort | robust and elastic lunar and martian structures from 3d-printed regolith inks |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5357966/ https://www.ncbi.nlm.nih.gov/pubmed/28317904 http://dx.doi.org/10.1038/srep44931 |
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