期刊
CERAMICS INTERNATIONAL
卷 47, 期 24, 页码 33956-33971出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.ceramint.2021.08.356
关键词
Ablation resistance; Thermal stability; Char residue; Ceramic particles; Phenolic resin; Carbon fiber
This review article provides a comparative analysis of researches in the field of ablative composites, discussing the performance improvement needs of carbon-phenolic composite systems and the effects of different additives on the properties of composite materials.
Ablative composites have been in use for thermal protection of space vehicles for decades. Carbon-phenolic composites have proven to perform exceptionally well in these applications. However with development in aerospace industry their performance needs improvement. In this field, different carbon-based and ceramic additives have been introduced into ablative composite systems. This review article gives a comparative analysis of researches done in this field in the recent past. Density, ablative, thermal and mechanical properties of ablative composites with different ultra-high temperature ceramic particles i.e. ZrSi2, Cenosphere, nano-SiO2, BN etc. and carbon-based nanoparticles i.e. CNTs, nano-Diamonds, Graphene oxide etc. used as additives, have been compared and discussed. Emphasis is put on carbon-phenolic composite systems although some epoxy matrix systems have also been discussed for comparison.
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