TY - JOUR
T1 - Probing Physicochemical Performances of 3D Printed Carbon Fiber Composites During 8-Month Exposure to Space Environment
AU - Di Trani, Nicola
AU - Masini, Attilio
AU - Bo, Tommaso
AU - Paci, Marco Maria
AU - Batra, Jaskirat Singh
AU - Reggiani, Maurizio
AU - Grattoni, Alessandro
N1 - Funding Information:
Part of this work was conducted at the Molecular Analysis Facility, a National Nanotechnology Coordinated Infrastructure (NNCI) site at the University of Washington, which is supported in part by funds from the National Science Foundation (awards NNCI‐2025489 and NNCI‐1542101), the Molecular Engineering & Sciences Institute, and the Clean Energy Institute. Funding support from the ISS National Laboratory (CASIS GA‐19‐003, PI Grattoni), the Houston Methodist Research Institute, and Automobili Lamborghini. Sample integration in the Space Development Acceleration Capability (SDAC) Flight Test Platform (FTP) was performed by Craig Technologies.
Publisher Copyright:
© 2023 The Authors. Advanced Functional Materials published by Wiley-VCH GmbH.
PY - 2024/3/25
Y1 - 2024/3/25
N2 - Carbon fiber reinforced polymers (CFRPs) offer exceptional properties that make them highly relevant in the aerospace industry, such as high thermal conductivity and an outstanding strength-to-weight ratio. Advances in additive manufacturing have expanded the aerospace applications of CFRPs, even allowing for in-space fabrication of complex structures. Understanding the stability of CFRPs in the harsh conditions of low Earth orbit (LEO) is crucial. LEO exposes materials to extreme environmental factors, such as vacuum, radiation, atomic oxygen, and temperature fluctuations, which can accelerate degradation. To investigate the space-environment effect on material, changes in properties of 3D-printed CFRPs are compared with CFRPs made through forging and conventional compression molding. Surface analyses examine morphological, chemical, and matrix composition changes, along with an evaluation of mechanical integrity. Remarkably, the naked 3D printed CFRPs withstood 8 months of LEO exposure similar to the compression molded CFRP samples, with changes in chemical properties limited to the sample's outer surface. Further, despite no protective coatings are used, limited surface erosion and no variation in mechanical strength are observed. These results provide relevant information for the development and deployment of novel 3D printed CFRPs materials for a wide spectrum of terrestrial and space applications.
AB - Carbon fiber reinforced polymers (CFRPs) offer exceptional properties that make them highly relevant in the aerospace industry, such as high thermal conductivity and an outstanding strength-to-weight ratio. Advances in additive manufacturing have expanded the aerospace applications of CFRPs, even allowing for in-space fabrication of complex structures. Understanding the stability of CFRPs in the harsh conditions of low Earth orbit (LEO) is crucial. LEO exposes materials to extreme environmental factors, such as vacuum, radiation, atomic oxygen, and temperature fluctuations, which can accelerate degradation. To investigate the space-environment effect on material, changes in properties of 3D-printed CFRPs are compared with CFRPs made through forging and conventional compression molding. Surface analyses examine morphological, chemical, and matrix composition changes, along with an evaluation of mechanical integrity. Remarkably, the naked 3D printed CFRPs withstood 8 months of LEO exposure similar to the compression molded CFRP samples, with changes in chemical properties limited to the sample's outer surface. Further, despite no protective coatings are used, limited surface erosion and no variation in mechanical strength are observed. These results provide relevant information for the development and deployment of novel 3D printed CFRPs materials for a wide spectrum of terrestrial and space applications.
KW - 3D printing
KW - CFRP
KW - ISS
KW - carbon fiber reinforced polymers
KW - low Earth orbit
KW - space
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U2 - 10.1002/adfm.202310243
DO - 10.1002/adfm.202310243
M3 - Article
AN - SCOPUS:85179660740
SN - 1616-301X
VL - 34
JO - Advanced Functional Materials
JF - Advanced Functional Materials
IS - 13
M1 - 2310243
ER -