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Thermophysical properties of hybrid silica phenolic ablative composite: Theoretical and experimental analysis
Polymer Composites ( IF 4.8 ) Pub Date : 2022-06-14 , DOI: 10.1002/pc.26766
Aravind Jithin A. J. 1, 2 , Sushanta K. Panigrahi 1 , Sasikumar P. 2 , Shreedhar K. Rao 2 , Shabeeb Ali T. K. 2 , Krishnakumar G. 2
Affiliation  

Silica phenolic ablative composites are used in many high-temperature applications like rocket/missile solid motor nozzles, space re-entry vehicles, and so forth. As ablative composite with lower thermal conductivity and density can save considerable cost, a hybrid silica phenolic ablative composite was developed by establishing a novel processing methodology using chopped silica fiber, phenolic resin, and hollow glass microsphere. The thermophysical properties of the developed hybrid composite are analyzed and established the scientific know-how. The developed composites, with 36% lower density, displayed 50% lower thermal conductivity and 50% lower thermal diffusivity than standard silica phenolic composite. Since a proper thermal conductivity model for a three-component composite with matrix, fiber, and hollow glass microsphere is not available, the most suitable model for the developed composite is established.

中文翻译:

杂化二氧化硅酚醛烧蚀复合材料的热物理性质:理论和实验分析

二氧化硅酚醛烧蚀复合材料用于许多高温应用,如火箭/导弹固体发动机喷嘴、太空再入飞行器等。由于具有较低导热率和密度的烧蚀复合材料可以节省大量成本,因此通过建立一种使用短切二氧化硅纤维、酚醛树脂和空心玻璃微球的新型加工方法,开发了一种混合二氧化硅酚醛烧蚀复合材料。对开发的杂化复合材料的热物理性质进行了分析,并建立了科学技术。与标准二氧化硅酚醛复合材料相比,开发的复合材料密度降低了 36%,热导率降低了 50%,热扩散率降低了 50%。由于没有合适的热导率模型用于具有基体、纤维和空心玻璃微球的三组分复合材料,
更新日期:2022-06-14
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