TY - JOUR
T1 - Laser-Induced Graphene Smart Textiles for Future Space Suits and Telescopes
AU - Yang, Dongwook
AU - Nam, Han Ku
AU - Lee, Younggeun
AU - Kwon, Soongeun
AU - Lee, Joohyung
AU - Yoon, Hyosang
AU - Kim, Young Jin
N1 - Publisher Copyright:
© 2024 The Author(s). Advanced Functional Materials published by Wiley-VCH GmbH.
PY - 2025/1/2
Y1 - 2025/1/2
N2 - Novel materials with high electrical, optical, and thermal functionalities are crucial in next-generation space missions. Astronauts’ well-being demands continuous health monitoring, while stray light suppression and heat dissipation are vital for space telescopes. Here, it is demonstrated that laser-induced graphene (LIG), patterned with femtosecond laser pulses, serves as a versatile material for temperature/strain sensing, stray light absorption, and heat management for smart spacesuits and telescopes. LIG exhibits a superior temperature coefficient of resistance (−0.068% °C⁻¹), gauge factor of 454, optical absorption (97.57%), and heat diffusivity (6.376 mm2 s−1) via a single platform. Furthermore, thermal-vacuum tests confirm LIG's reliability and readiness for space missions. Under vacuum conditions (≈10−3 Torr) and repeated temperature changes ranging from −20 to 60 °C over a period of ≈40 h, the temperature/strain sensor, and optical absorbers maintain the functionality.
AB - Novel materials with high electrical, optical, and thermal functionalities are crucial in next-generation space missions. Astronauts’ well-being demands continuous health monitoring, while stray light suppression and heat dissipation are vital for space telescopes. Here, it is demonstrated that laser-induced graphene (LIG), patterned with femtosecond laser pulses, serves as a versatile material for temperature/strain sensing, stray light absorption, and heat management for smart spacesuits and telescopes. LIG exhibits a superior temperature coefficient of resistance (−0.068% °C⁻¹), gauge factor of 454, optical absorption (97.57%), and heat diffusivity (6.376 mm2 s−1) via a single platform. Furthermore, thermal-vacuum tests confirm LIG's reliability and readiness for space missions. Under vacuum conditions (≈10−3 Torr) and repeated temperature changes ranging from −20 to 60 °C over a period of ≈40 h, the temperature/strain sensor, and optical absorbers maintain the functionality.
KW - direct laser writing
KW - laser-induced graphene
KW - smart textile
KW - space-qualified
UR - https://www.scopus.com/pages/publications/85206622550
U2 - 10.1002/adfm.202411257
DO - 10.1002/adfm.202411257
M3 - Article
AN - SCOPUS:85206622550
SN - 1616-301X
VL - 35
JO - Advanced Functional Materials
JF - Advanced Functional Materials
IS - 1
M1 - 2411257
ER -