<HashMap><database>biostudies-literature</database><scores/><additional><submitter>Zhao X</submitter><funding>Shandong Provincial Natural Science Foundation</funding><pagination>387</pagination><full_dataset_link>https://www.ebi.ac.uk/biostudies/studies/S-EPMC12899982</full_dataset_link><repository>biostudies-literature</repository><omics_type>Unknown</omics_type><volume>18(3)</volume><pubmed_abstract>To meet the requirements of next-generation spacecraft thermal protection systems for lightweight materials with high strength, effective thermal insulation, and superior ablation resistance, a novel POSS-modified phenolic aerogel/quartz fiber composite (POSS-PR/QF) was developed using a thiol-ene click reaction combined with a sol-gel process. Covalent incorporation of polyhedral oligomeric silsesquioxanes (POSS) into the phenolic matrix effectively eliminates nanoparticle aggregation and improves interfacial compatibility. As a result, the modified resin is suitable for resin transfer molding (RTM) processes. The resulting composite exhibited an aerogel-like porous structure with enhanced crosslinking density, thermal stability, and oxidation resistance. At 7.5 wt% POSS loading, the composite achieved low density (~0.7 g·cm&lt;sup>-3&lt;/sup>) and outstanding mechanical properties, with tensile, flexural, compressive, and interlaminar shear strengths increased by 114%, 79%, 29%, and 104%, respectively. Its thermal conductivity (0.0619 W/(m·K)) and ablation rates were also markedly reduced. Mechanistic studies revealed that POSS undergoes in situ ceramification to form SiO&lt;sub>2&lt;/sub> and SiC phases, which create a dense protective barrier. In addition, this ceramification process promotes char graphitization, thereby enhancing oxidation resistance and thermal insulation. This work provides a promising approach for designing lightweight, high-performance, and multifunctional thermal protection materials for aerospace applications.</pubmed_abstract><journal>Polymers</journal><pubmed_title>Preparation of Phenolic Aerogel/Quartz Fiber Composites Modified with POSS: Low Density, High Strength and Thermal Insulation.</pubmed_title><pmcid>PMC12899982</pmcid><funding_grant_id>ZR2024QE229</funding_grant_id><pubmed_authors>Ren X</pubmed_authors><pubmed_authors>Liu J</pubmed_authors><pubmed_authors>Liu Z</pubmed_authors><pubmed_authors>Fan X</pubmed_authors><pubmed_authors>Feng J</pubmed_authors><pubmed_authors>Li D</pubmed_authors><pubmed_authors>Yu Q</pubmed_authors><pubmed_authors>Shao M</pubmed_authors><pubmed_authors>Yu G</pubmed_authors><pubmed_authors>Yuan W</pubmed_authors><pubmed_authors>Zhao X</pubmed_authors><pubmed_authors>Kong G</pubmed_authors></additional><is_claimable>false</is_claimable><name>Preparation of Phenolic Aerogel/Quartz Fiber Composites Modified with POSS: Low Density, High Strength and Thermal Insulation.</name><description>To meet the requirements of next-generation spacecraft thermal protection systems for lightweight materials with high strength, effective thermal insulation, and superior ablation resistance, a novel POSS-modified phenolic aerogel/quartz fiber composite (POSS-PR/QF) was developed using a thiol-ene click reaction combined with a sol-gel process. Covalent incorporation of polyhedral oligomeric silsesquioxanes (POSS) into the phenolic matrix effectively eliminates nanoparticle aggregation and improves interfacial compatibility. As a result, the modified resin is suitable for resin transfer molding (RTM) processes. The resulting composite exhibited an aerogel-like porous structure with enhanced crosslinking density, thermal stability, and oxidation resistance. At 7.5 wt% POSS loading, the composite achieved low density (~0.7 g·cm&lt;sup>-3&lt;/sup>) and outstanding mechanical properties, with tensile, flexural, compressive, and interlaminar shear strengths increased by 114%, 79%, 29%, and 104%, respectively. Its thermal conductivity (0.0619 W/(m·K)) and ablation rates were also markedly reduced. Mechanistic studies revealed that POSS undergoes in situ ceramification to form SiO&lt;sub>2&lt;/sub> and SiC phases, which create a dense protective barrier. In addition, this ceramification process promotes char graphitization, thereby enhancing oxidation resistance and thermal insulation. This work provides a promising approach for designing lightweight, high-performance, and multifunctional thermal protection materials for aerospace applications.</description><dates><release>2026-01-01T00:00:00Z</release><publication>2026 Jan</publication><modification>2026-07-07T03:16:20.921Z</modification><creation>2026-07-07T03:08:46.444Z</creation></dates><accession>S-EPMC12899982</accession><cross_references><pubmed>41682094</pubmed><doi>10.3390/polym18030387</doi></cross_references></HashMap>