3D Printing of Liquid Crystal Polymers for Space Applications
C.C.M.C.A.G. Houriet (TU Delft - Aerospace Engineering)
Evelien Claassen (Student TU Delft)
Chiara Mascolo (NematX AG)
Haimo Jöhri (Paul Scherrer Institute)
Abel Brieva (European Space Research and Technology Centre)
Szilvia Szmolka (European Space Research and Technology Centre)
Sebastien Vincent-Bonnieu (European Space Research and Technology Centre)
Agnieszka Suliga (European Space Research and Technology Centre)
Kunal Masania (TU Delft - Aerospace Engineering)
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Abstract
Fused Filament Fabrication is a promising manufacturing technology for the circularity of space missions. Potential scenarios include in-orbit applications to maximize mission life and to support long-term exploration missions with in situ manufacturing and recycling. However, its adoption is restricted by the availability of engineering polymers displaying mechanical performance combined with resistance to space conditions. Here, a thermotropic Liquid Crystal Polymer (LCP) is reported as a candidate material with extrusion 3D printing. To expand its scope of applicability to structural parts for space applications, four different exposure conditions are studied: thermal cycling under vacuum, atomic oxygen, UV, and electron irradiations. While 1 MeV-electron irradiation leads to a green coloration due to annealable color centers, the mechanical performance is only slightly decreased in dynamic mode. It is also found that increased printing temperature improves transverse strength and resistance to thermal cycling with the trade-off of tensile stiffness and strength. Samples exposed to thermal cycling and the highest irradiation dose at lower printing temperatures still display a Young's modulus of 30 GPa and 503 MPa of tensile strength which is exceptionally high for a 3D-printed polymer. For the types of exposure studied, overall, the results indicate that LCP 3D-printed parts are well suited for space applications.
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