Developing lightweight and efficient ablation-resistant materials with thermal insulation and
conformability over 2500° C is extremely important for the thermal protection of hypervelocity …

Abstract Thermal Protection Systems (TPS) material response models rely on the
assumption of local thermal equilibrium (LTE) between the solid phase and the gas phase …

This works discusses the high temperature decomposition of Room Temperature Vulcanized
(RTV) silicone, an adhesive material used as a gap filler in ablative heatshield for planetary …

The present work innovatively investigates the one-sided flame heating thermal response
and pyrolysis behavior of carbon fiber/phthalonitrile (Cf/PN) composite laminates. The …

This study explores the suitability of hydrogen-based plasma in direct power extraction
(DPE) as a non-conventional electricity generation method. We apply computational …

Abstract Carbon/carbon (C/C) composites as one of thermal protection materials for
hypersonic vehicles are subjected to extreme thermochemical ablation and mechanical …

Deep space exploration is a significant focus in the aerospace field, encompassing missions
to celestial bodies such as Mars, Venus, and beyond. During exploration, the thermal …

View Video Presentation: https://doi. org/10.2514/6.2023-2720. vid Mars 2020 was protected
during atmospheric entry by a heatshield made of Phenolic Impregnated Carbon Ablator …

The inclusions in a high-temperature resistant matrix can significantly influence the radiative
heat transfer of composite materials at elevated temperatures; therefore, the microstructure …

View Video Presentation: https://doi. org/10.2514/6.2023-0962. vid The objective of this work
was to assess the impact of flow field-material response coupling on reproducing …