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Short silica fibre-reinforced polymethylsilsesquioxane-phenolic interpenetrating networks: exploration for use as ablative thermal protection system in aerospace

机译:短二氧化硅纤维增强的聚甲基硅酸辛硅氧烷 - 酚醛渗透网络:在航空航天中用作烧蚀热保护系统的探索

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摘要

Short silica fibre-reinforced simultaneous interpenetrating polymer network (IPN) composites consisting of polymethylsilsesquioxane (PMSQ) and phenol-formaldehyde resin were prepared through thermal cross-linking. Such IPN composites combine the advantageous ablative features of individual systems and excellent thermal insulation aspects. IPNs were prepared with varying composition between PMSQ and PF, at constant fibre content (60% by weight). The influence of IPN composition on the ablation and out-gassing characteristics was explored in detail. Arc-jet evaluation brought out the superior thermal shock resistance of IPN composites that were richer in PMSQ content. Further, it was inferred that the mechanism of thermal protection shifted to ablative heat shielding with increase in PF content. Microstructural characterization of the arc plasma eroded specimens was carried out using FTIR and Raman spectroscopy to understand the chemical mechanism of erosion process. Higher PMSQ content facilitated the formation of SiOC glass, whereas higher PF content resulted in well-defined char layer comprised of predominantly pyrolytic carbon. Higher PMSQ content also favoured lower out-gassing properties. The study brought out the superior thermal protection capability of the IPN with respect to aerospace applications.
机译:通过热交联制备由聚甲基羟基硅氧烷(PMSQ)和酚醛树脂组成的短二氧化硅纤维增强的同时互穿互穿的聚合物网络(IPN)复合材料。这种IPN复合材料结合了各个系统的有利烧蚀特征和优异的隔热方面。在PMSQ和PF之间的不同组成,在恒定纤维含量(60重量%)之间制备IPN。探讨了IPN组成对烧蚀和外阴特性的影响。 Acc-Jet评估为PMSQ含量富有更丰富的IPN复合材料的卓越热抗震性。此外,推断出热保护机理转移到烧蚀热屏蔽,随着PF含量的增加。使用FTIR和拉曼光谱进行电弧等离子体侵蚀标本的微观结构表征,了解侵蚀过程的化学机理。较高的PMSQ含量促进了SIOC玻璃的形成,而较高的PF含量导致由主要的热解碳组成的明确定义的炭层。较高的PMSQ含量也有利于降低流出性的特性。该研究为航空航天应用提供了IPN的卓越的热保护能力。

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