Abstract

Additive manufacturing (AM) is one of the most promising techniques for on-site manufacturing on extraterrestrial bodies. In this investigation, layerwise solar sintering under ambient and vacuum conditions targeting lunar exploration and a moon base was studied. A solar simulator was used in order to enable AM of interlockable building elements out of JSC-2A lunar regolith simulant. Solar additively manufactured samples were characterized mechanically regarding their compressive and bending properties. Moreover, samples were analyzed morphologically using X-ray tomography and scanning electron microscopy (SEM) followed by density measurements. AM for identical process parameters led to final products with different physical and chemical characteristics when performed under ambient and vacuum conditions. Hence, process parameters were optimized under each individual working atmosphere. The experimental data were further integrated into finite-element (FE) calculations. This led to the refinement of the design of interlocking building elements for lunar applications. These blocks have the potential to form structures for shielding a pressurized inflatable habitat from radiation and micrometeorite impacts or creating nonpressurized shelters for robotic machinery.

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Acknowledgments

Project RegoLight has received funding from the European Union’s Horizon 2020 research and innovation program under Grant Agreement No. 686202. The authors wish to thank Martin Thelen, Christian Willsch, Christian Raeder, Hans-Gerd Dibowski, Joseph Salini, Matthias Kolbe, Olfa Lopez, Anthony Rawson, and Valerie Morisseaux for their support during the test campaigns in Deutsches Zentrum für Luft- und Raumfahrt (DLR)-Cologne.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 32Issue 6November 2019

History

Received: Nov 21, 2018
Accepted: Jun 21, 2019
Published online: Sep 14, 2019
Published in print: Nov 1, 2019
Discussion open until: Feb 14, 2020

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Miranda Fateri, Ph.D. [email protected]
Research Fellow, Institut für Materialphysik im Weltraum, Deutsches Zentrum für Luft- und Raumfahrt, Köln 51170, Germany (corresponding author). Email: [email protected]
Alexandre Meurisse, Ph.D. https://orcid.org/0000-0001-8955-6926
Research Fellow, Institut für Materialphysik im Weltraum, Deutsches Zentrum für Luft- und Raumfahrt, Köln 51170, Germany. ORCID: https://orcid.org/0000-0001-8955-6926
Matthias Sperl, Ph.D.
Professor, Institut für Materialphysik im Weltraum, Deutsches Zentrum für Luft- und Raumfahrt, Köln 51170, Germany.
Diego Urbina
Team Lead, Future Projects and Exploration, Space Applications Services, Leuvensesteenweg 325, Zaventem, Brussel 1932, Belgium.
Hemanth Kumar Madakashira
Systems Engineer, Future Projects and Exploration, Space Applications Services, Leuvensesteenweg 325, Zaventem, Brussel 1932, Belgium.
Shashank Govindaraj
Team Leader, Robotics Software, Space Applications Services, Leuvensesteenweg 325, Zaventem, Brussel 1932, Belgium.
Jeremi Gancet, Ph.D.
Division Manager, Technologies, Applications and Research, Space Applications Services, Leuvensesteenweg 325, Zaventem, Brussel 1932, Belgium.
Team Lead, LIQUIFER Systems Group, Obere Donaustraße 97-99/1/62, Vienna 1020, Austria. ORCID: https://orcid.org/0000-0001-5968-1929
Waltraut Hoheneder
Design Engineer, LIQUIFER Systems Group, Obere Donaustraße 97-99/1/62, Vienna 1020, Austria.
René Waclavicek
Design Engineer, LIQUIFER Systems Group, Obere Donaustraße 97-99/1/62, Vienna 1020, Austria.
Clemens Preisinger, Ph.D.
Senior Engineer, Bollinger und Grohmann GmbH, Franz-Josefs-Kai 31/1/4, Frankfurt am Main 60327, Germany.
Emilio Podreka, Ph.D.
Senior Engineer, Bollinger und Grohmann GmbH, Franz-Josefs-Kai 31/1/44, Frankfurt am Main 60327, Germany.
Makthoum Peer Mohamed
Aerospace Engineer, Compagnie Maritime d’Expertise, 36 Blvd. de l’Océan, Marseille 13009, France.
Peter Weiss, Ph.D.
Team Lead, Compagnie Maritime d’Expertise, 36 Blvd. de l’Océan, Marseille 13009, France.

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