TY - JOUR
T1 - Anti-ablation and insulation integrated gradient quartz fiber needle felt reinforced SiO2 ceramic/aerogel composite for thermal protection
AU - Xu, Kai
AU - Wu, Chongying
AU - Chen, Zhaofeng
AU - Liu, Hongwei
AU - Li, Manna
AU - Yang, Lixia
AU - Ai, Sufen
AU - Cui, Sheng
N1 - Publisher Copyright:
© 2024 Elsevier Ltd and Techna Group S.r.l.
PY - 2025/1
Y1 - 2025/1
N2 - Amidst the rigorous thermal challenges faced by hypersonic vehicles, this study introduces a quartz fiber needle felt-reinforced SiO₂ ceramic/aerogel (QF-SA) composite, demonstrating exceptional thermal protection capabilities. Under a quartz lamp, the composite maintained surface temperatures at 800 °C after an initial spike to 1000 °C, with backing plate temperatures peaking at 232 °C after 1000 s for the QF-SA1 variant. Its thermal conductivity, which ranges from 0.022 to 0.042 W/m·K, offers optimized insulation. Laser ablation tests at 3 kW for 9s revealed outstanding durability, with mass and linear ablation rates of 0.0068 ± 0.0002 g/s and 1.5 ± 0.1 mm/s for QF-SA3, respectively—45.6 % and 31.9 % lower than those of QF-A. These results highlight the QF-SA composites potential for high-temperature aerospace applications, indicating a path forward for lightweight, high-performance thermal protection systems. Future work will focus on refining fabrication techniques to achieve optimal performance and address economic constraints.
AB - Amidst the rigorous thermal challenges faced by hypersonic vehicles, this study introduces a quartz fiber needle felt-reinforced SiO₂ ceramic/aerogel (QF-SA) composite, demonstrating exceptional thermal protection capabilities. Under a quartz lamp, the composite maintained surface temperatures at 800 °C after an initial spike to 1000 °C, with backing plate temperatures peaking at 232 °C after 1000 s for the QF-SA1 variant. Its thermal conductivity, which ranges from 0.022 to 0.042 W/m·K, offers optimized insulation. Laser ablation tests at 3 kW for 9s revealed outstanding durability, with mass and linear ablation rates of 0.0068 ± 0.0002 g/s and 1.5 ± 0.1 mm/s for QF-SA3, respectively—45.6 % and 31.9 % lower than those of QF-A. These results highlight the QF-SA composites potential for high-temperature aerospace applications, indicating a path forward for lightweight, high-performance thermal protection systems. Future work will focus on refining fabrication techniques to achieve optimal performance and address economic constraints.
KW - Aerogel
KW - Ceramic-matrix composites (CMCs)
KW - Thermal analysis
KW - Thermal properties
UR - http://www.scopus.com/inward/record.url?scp=85209063305&partnerID=8YFLogxK
U2 - 10.1016/j.ceramint.2024.11.186
DO - 10.1016/j.ceramint.2024.11.186
M3 - 文章
AN - SCOPUS:85209063305
SN - 0272-8842
VL - 51
SP - 2094
EP - 2103
JO - Ceramics International
JF - Ceramics International
IS - 2
ER -