Chen QiuJiemin LuoYouquan LingZhao‐Hui LuLong NiYang ChenHuawei ZouZhengguang HengMei Liang
Abstract Organosilicon modified epoxy resin is one of the most widely used ablative coating matrices in the whole aerospace industry. However, most research focuses on the final effect of organosilicon modification, while systematic studies on thermal degradation behavior and mechanism of organosilicon modified epoxy resin are rarely reported. In this work, a heat‐resistant epoxy resin (ES231) is prepared through the condensation reaction between epoxy resin and methylphenyl organosilicon intermediate. The TGA test results show that the integral procedural decomposition temperature (IPDT), the thermal residual weight at 800 °C (R 800 ), and decomposition temperature range all improve under both N 2 and air atmospheres after modification. The functional groups variation of polymers and the generated volatile segments during the degradation process are measured by FTIR, TG‐IR, and TG‐MS to investigate the thermal degradation mechanism in detail. Meanwhile, the composition and microstructure of the solid residue after thermal degradation are also systematically studied by SEM, XPS, and Raman spectroscopy. It is expected that this work can provide some theoretical basis and new ideas for designing new heat‐resistant epoxy resin.
Xiaohui BaoFangyi WuJiangbo Wang
Meili CuiLili ZhangPingping LouXuezhong ZhangXiaojie HanZhijie ZhangShuhua Zhu
Mohammad Hossein KaramiMohammadreza KalaeeRamin KhajaviOmid MoradiDavood Zaarei
Xiaojun HuYa Nan ChenQing BianMing ChenWen QinJing Feng