气凝胶
材料科学
复合材料
电磁干扰
电磁屏蔽
复合数
电磁干扰
陶瓷
航空航天
多孔性
热的
航天器
烧蚀
碳纳米管
弹性(物理)
变形(气象学)
保温
比模量
复合材料层合板
光电子学
作者
Yu Guan,Congke Gu,Guofang Qiu,Jiahui Wu,Xizheng Lian,Xin Wang,Bin Jun Fei,Wei Wang,Diantang Zhang,Wenwen Guo
标识
DOI:10.1002/adfm.202528431
摘要
ABSTRACT The rapid advancement of space science and technology poses severe challenges for deep space probes operating in extreme thermo‐electromagnetic environments. However, traditional rigid aerospace materials lack sufficient deformation adaptability and cannot integrate thermal protection with electromagnetic interference (EMI) shielding. To overcome these limitations, we developed a Triple‐Network aerogel composite with thermally induced “Phoenix‐like” transformation, which was fabricated through a molecular‐scale covalent‐coordination strategy. The resulting titanium‐boron‐silicon phenolic aerogel (T‐BS‐PRf) features a triple cross‐linked interpenetrating network, which gives it an ultralow density of ≈0.204 g/cm 3 , excellent elasticity (>92% recovery at 50% strain), and a strength of 1.97 MPa and overcomes the typical strength–elasticity trade‐off. The composite also exhibits outstanding thermal insulation and ablation resistance, maintaining structural integrity with a very low linear ablation rate of 0.00279 mm/s after 30 min under a 1300°C flame. Notably, ablation triggers an in situ ceramic transformation, yielding a porous carbon aerogel (T‐BS‐Cf) that provides outstanding EMI shielding (92.8 dB in the X‐band) and retains robust mechanical properties (8.62 MPa strength, elasticity recovery 94.7% at 40% strain). This work successfully integrates high elasticity, extreme thermal protection, and effective EMI shielding in a single composite, offering a new design strategy for multifunctional spacecraft in extreme environments.
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