1. Introduction
Fig. 1. Preparation methods, macroscopic morphologies, microstructures, and resilient compressibility of flexible nanostructures assembled ceramic aerogels. (a) Blow spinning prepared TiO2 nanofiber aerogel [17] Copyright © 2017, The American Association for the Advancement of Science. (b) Chemical vapor deposition synthesized SiC nanowire aerogel [19] Copyright © 2018, American Chemical Society. (c) Freeze-drying assembled SiO2 nanowire aerogel [18] Copyright © 2018, The American Association for the Advancement of Science. (d) Electrospinning induced ZrO2 ceramic nanofiber aerogel [25] Copyright © 2022, The Author(s). |
Table 1. Quantitative performance benchmarks and extreme-environment tolerance of representative ceramic aerogels. |
| Material system | Architecture | Density (mg/cm³) | Compressive strength (kPa) / strain | Tensile strength (kPa) | Thermal conductivity (mW·m⁻¹·K⁻¹) | Max service temp (°C, air/inert) | Fatigue cycles (strain retention) | Thermal shock resistance (ΔT, cycles) | CEF | Refs. |
|---|---|---|---|---|---|---|---|---|---|---|
| Laminated SiC nanowire | Lamellar | 50 | 1255 @80% | 400 | 39 (⊥) | 1200 / 1400 | 100 (90%) | -196~800°, 100× | 20.01 | [30] |
| Laminated Si3N4 | Lamellar | 200 | 176,350 @97% | N/A | 83.2 | 1000 / 1400 | N/A | N/A | 275.5 | [31] |
| Dome-celled high-entropy carbide | Dome-celled | 0.35~13.78 | 300~18000 @99% | N/A | 12-15 | 1200 / 2000 | 20,000 (99%) | 4.2~2273 K, >50× | >45 | [37] |
| Bouligand mullite | Bouligand | 200~330 | 156 @80% | 170,380 | 37-76 | 1200/ 1200 | N/A | N/A | 3.1 | [61] |
| Curly SiC-SiOx | Helical | ~5.7 | 28 @80% | 30 (strain) | 28.4 | 600 / 1200 | 100 (98%) | N/A | 2.7 | [32] |
| Double-crosslinked PI-SiO2 | Hybrid interpenetrating | ~250 | 65,600 @80% | 8,500 (54% strain) | 35 | 300/300 | N/A | N/A | 58.5 | [45] |
| Si3N4@SiO2 core-shell | Core-shell random | 20 | 27 @80% | N/A | 29 | 1300 / 1300 | 100 | 25~1300°C, 100× | 1.6 | [40] |
| High-entropy oxide ZLSGY | Random + crosslink | 5~50 | 229 @98% | 11 (52% strain) | ~25 | 1400 / 1400 | 1000 (<3% loss) | 25~1400°C cyclic | 13.3 | [86] |
| Polyimide nanofibrous (PINA) | Lamella-crosslinked | 7.6 | 12 @75% | N/A | 26.4 | 300 / 300 | 10,000 (97%) | -196~300°C | 0.5 | [47] |
| Hierarchical dual-oxide nanofiber | Hierarchical | 8 | 8 @90% | - | 7 | 1200/1200 | 100 | -196 ~1300°C | 4.7 | [79] |
Table 2. Comparison of design strategies and mechano-thermal synergy for elastic ceramic aerogels. |
| Strategy category | Specific architecture | Materials | Mechanical performance | Thermal conductivity (mW·m-1·K-1) | Service temperature range (air/inert, °C) | Refs. |
|---|---|---|---|---|---|---|
| Network architecture | Lamellar | SiC, Si3N4 | Compressive strength 1 MPa, recovery 80%(SiC); >170 MPa, 97% deformation (Si3N4) | 35-85 | 1500°C / 1200 | [30], [31] |
| Honeycomb / dome-celled | High-entropy carbide | Compressive strength 0.3-18 MPa; recovery >99% (up to 2273 K) | 12-170 | 1200 / 2000 | [37] | |
| Bouligand (chiral) | Mullite | Compressive 156 kPa, recovery >90%; tensile stress 170 MPa; | 37-76 | 1200 / 1200 | [61] | |
| Helical / buckled | SiC-SiOx | Compressive <50 kPa; tensile strain up to 20% | ~25 | 1000 /1500 | [32], [34] | |
| Interfacial engineering | Core-shell (SiO2 shell) | Si3N4@SiO2 | 27 kPa @80% compressive strain | 29~35 | 1300 / 1300 | [40], [60] |
| Core-shell (PyC shell) | BN@PyC | Tunable (superelastic to rigid) | Tunable thermal conductivity | 500 / 1400 | [39], [71] | |
| Dual-phase nodes (PyC+ SiO2) | SiC nanowire | Compressive 10.9 MPa @80% strain; recovery ~80% | ~38 | 500 / 1400 | [41] | |
| Multi-scale composite | Gradient impedance | SiC/Si3N4 | Maintains mechanical integrity with microwave absorption | Gradient insulation | Depends on components | [72] |
| Sandwich | Ceramic nanofiber | Compressive strength 249 kPa @80% strain; Tensile strength 565 kPa | Core insulation; dense skin barrier | Depends on skin/core | [43] | |
| Hierarchical | Nacre-mimetic, dual-oxide nanofiber | High stiffness + superelasticity + bending flexibility | 7~24 | -196 to 1200 | [42], [78], [79] | |
| Hybrid interpenetrating network | PI- SiO2 double-crosslinked | Compressive 65.6 MPa @80% strain; tensile 8.5 MPa; record toughness | ~35 | -110 to 300 / 400 | [45] |
Table 3. Thermal stability and service boundaries of different material systems. |
| Material system | Representative example | Max service temp in air (°C) | Max service temp in inert (°C) | Degradation mechanism | Recommended environment | Best-suited architecture | Refs. |
|---|---|---|---|---|---|---|---|
| Oxide (fully ceramic) | Mullite, Al2O3, ZrO2 | 900-1300 | 1400+ | Sintering >1000°C | Air up to 1200°C | Lamellar, anisotropic aligned | [28], [59] |
| Non-oxide (carbide, nitride) | SiC, Si3N4, BN | <600 (uncoated) | 1400+ | Oxidation to oxide layer (passivating but brittle) | Inert or vacuum >600°C | Honeycomb, dome-celled | [19], [27] |
| Core-shell (oxide shell on non-oxide core) | SiC@SiO2, Si3N4@SiO2 | 1200 | 1400+ | SiO2 sintering >1000°C; shell protects core | Air up to 1200°C | Random network, lamellar | [40], [60] |
| High-entropy ceramic | (LaSmGdY)2Zr2O7, (HfZrTaNb)C | 1400 (oxide); <600 (carbide, uncoated) | 1400+ | Grain growth suppressed; high oxidation resistance for oxides | Air (oxides); inert (carbides) | Dome-celled, Bouligand | [37], [86] |
| Carbon-containing ceramic | SiC@PyC, graphene-SiC | 400-500 | 1400+ | PyC/graphene oxidizes >400°C | Inert or vacuum >500°C | Any (with protective coating if needed) | [38], [41] |
| Organic-inorganic hybrid | PI-SiO2 double-crosslinked | 400 | 400 | Polymer decomposition >400°C | Low-temperature air | Sandwich, interpenetrating network | [44], [45] |
Fig. 2. Illustration of the contents in this review. Reproduced with permission from Ref. [37], [42], [43], [59], [60], [61], [62] Copyright © 2025, The American Association for the Advancement of Science, © 2023 Wiley‐VCH GmbH, Copyright, © 2025 Elsevier B.V. All rights are reserved, including those for text and data mining, AI training, and similar technologies, © 2020, American Chemical Society, © 2023 Elsevier Ltd. All rights reserved, Copyright © 2024, The Author(s), © 2025 Wiley‐VCH GmbH. |
2. Foundational Building Blocks for Mechanical Optimization
2.1. Nanowires and Nanofibers: The Pillars of Resilience
2.2. Nanorods and Nanosheets: Expanding the Design Space
2.3. Impact on Deformation Mechanisms
Fig. 3. Deformation mechanisms of resilient ceramic aerogels during compression and stretch. (a) Microstructure evolution of SiC nanowire aerogel during reversible compression [19] Copyright © 2018, American Chemical Society. (b) Macroscopic morphology evolution, compressive stress-strain curve, and (c) microstructure evolution of Si3N4 nanobelt aerogel [27] Copyright © 2019, American Chemical Society. (d) Tensile deformation mechanisms and (e) tensile stress-strain curve of resilient curly SiC-SiOx nanowire aerogel [32] Copyright © 2021, American Chemical Society. (f) Microstructure evolution of spiral crimped Janus nanofibers in ceramic aerogel and (g) the corresponding stress-strain curve [67]. (h) Structure design of curly nanofiber in ceramic aerogels. (i) Deformation behaviors of straight and curly nanofiber aerogels [34] © 2024 Wiley‐VCH GmbH. |
3. Structural Design for Enhanced Mechanical Performance
Fig. 4. Mechanical and thermal properties of a laminated SiC nanowire aerogel [30] Copyright © 2023, The Author(s). (a) The preparation process. (b) Microstructures with laminated distribution of nanowires and interweaving nanowires in each laminate. (c) Deformation behavior of the aerogel. (d) Compressive stress-strain curve. (e) Tensile stress-strain curve. (f-h) Anisotropic thermal conducting behavior of the aerogel. (i) Thermal insulation behavior of the aerogel. |
Fig. 5. Cellular structure design for high strength, ultrahigh temperature thermal stability, thermal insulation and thermal shock resistance [37] Copyright © 2025, The American Association for the Advancement of Science. |
Fig. 6. Bouligand structure design for simultaneously high compressive strength, high tensile strength, and thermal insulation performance [61] Copyright © 2024, The Author(s). (a) The preparation process. (b) Microstructures of BcF-CAs. (c) Deformation behavior of the aerogel. (d) Compressive stress-strain curve. (e) Tensile stress-strain curve. (f) Thermal conducting behavior of the aerogel. |
4. Interfacial Engineering and Node Reinforcement
Fig. 7. Interfacial engineering and node reinforcement for improved mechanical properties. (a) Interfacial cross-linking by using SiO2 interfacial bonding [70] Copyright © 2021, American Chemical Society. (b) Zr-O-Si glass modification [62] © 2025 Wiley‐VCH GmbH. (c) Surface SiO2 coating for core-shell structure [60] © 2023 Elsevier Ltd. All rights reserved. (d) Soft carbon and hard SiO2 dual phase structure for high compressive strength [41]. |
5. Multi-Scale Strategy for Multifunction
Fig. 8. Multiscale structure design for improved mechanical and thermal performance. (a) SEM images of cross section and enlarged views of different zones for MF15/AR-C50. (b) The compressive stress-strain profiles. (c) Photograph of the quartz lamp simulation experiment (inset) and cold-side temperature rise-time curves of MF15/AR-C10 and mullite fiber at 1500 °C for 900 s [74] © 2023 Elsevier B.V. All rights reserved. (d) SEM image of the sandwich structure in S-CNFAs. (e) Compressive σ−ε curves. (f) Tensile σ−ε curve of S-CNFAs [43] © 2025 Elsevier B.V. All rights are reserved, including those for text and data mining, AI training, and similar technologies. (g) SEM analysis of SCQ aerogels. (h) The compressive stress-strain curves. (i) Photographs and infrared images of SCQs exposed to the flame of an alcohol lamp [42] © 2023 Wiley‐VCH GmbH. (j) Section morphology of tensile fracture of PIACs with different SiO2 content. (k) Tensile stress-strain curves. (l) Diagram of a test device for membranes from high to cryogenic temperature. e) Low temperature thermal insulation performance test of PIAC with different layers [45] © 2025 Wiley‐VCH GmbH. |
6. Performance Under Extreme Conditions
Fig. 9. Performance of aerogels under extreme conditions. Reproduced with permission from Ref.[22], [25], [34], [42], [47], [48], [51] © 2020 Wiley‐VCH GmbH, Copyright © 2022, The Author(s), © 2024 Wiley‐VCH GmbH, © 2023 Wiley‐VCH GmbH, Copyright © 2025, American Chemical Society, Copyright © 2025, American Chemical Society. |
