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  • A novel concept for in-situ manufacture of reinforced sintered construction elements and a numerical assessment of material properties

    Paper number

    IAC-16,A3,2B,10,x32044

    Author

    Mr. Francesco Spina, ESA european space agency, Germany

    Coauthor

    Mr. Alberto Canals Pou, European Space Agency (ESA), Spain

    Coauthor

    Mr. Marc Villa Montero, Alpha STAR Corporation, United States

    Coauthor

    Dr. Aidan Cowley, ESA european space agency, Germany

    Coauthor

    Mr. Leo Teeney, ESA, Germany

    Coauthor

    Mr. Alexandre Meurisse, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany

    Year

    2016

    Abstract
    Reduction of future mission payload mass by exploiting In-Situ Resource Utilization (ISRU) approaches is vital to build sustainable extra-terrestrial bases. The sintering of planetary regolith has been proposed by many researchers as an ISRU test case with architectural or structural applications (landing pads, micrometeorite protection, etc.). However, research with terrestrial regolith simulants has shown that sintered regolith does not have a high tensile strength, potentially reducing its use to applications with low tensile loads. This paper details a conceptual system designed to exploit Lunar regolith and convert it into structural elements for future planetary exploration missions. It has been previously shown that fiberglass can be produced by using extrusive igneous basalt soil. Therefore, it could be used as reinforcement for sintered regolith blocks. We outline a novel yet simple process to fabricate reinforced blocks with multiple use case scenarios as well as realistic Technology Readiness Level (TRL) requirements to implement such a system. Using information derived experimentally and available in literature, computational simulations have been carried out, showing significant material enhancement properties for building elements fabricated using our proposed fiberglass approach. It has been determined that using a [0/90] configuration for the fibers, the longitudinal strength of the composite would increase by a factor of six.
    Abstract document

    IAC-16,A3,2B,10,x32044.brief.pdf

    Manuscript document

    (absent)