The research that will be performed will be testing thermal coating for composite material for aircraft flying at higher speeds. We will be testing a different variation of composite material to test which variation has the lowest thermal conductivity reducing the rate of heat absorbed to the interior, preventing any harm dealt with the structural integrity at the aircraft's interior. With the current generation of aircraft, the thermal coating consists of ceramic powder with good heat transfer capabilities and can withstand high amounts of heat, but this ceramics powder makes the aircraft heavier and expensive. New forms of thermal coating are needed for newer aircraft like the Boeing Starliner 787, mainly constructed out of carbon-fiber material. The benefits of carbon fiber include making craft light, reducing cost, and enabling greater distance flight. In this research, we will be investigating the material integrity under various stress to see whether it will withstand the intense stress it will be put as the craft flies at high speeds (possible match speeds). This research is significant as newer generation passengers are integrated; most of it is a composite material. As such thermal coating on the plane will need to show low heat-conductive transfer and low thermal conductivity as carbon composite does not have high thermal properties at higher temperatures. This research will be to find and test material that shows these properties so that structure of the plane will not be damaged due to heat generated due to air friction. As there have been various research that has been realized on testing various composite materials showing their heat capabilities, but most of these papers show whether they have good heat conductivity transfer, as this research will provide more detail on to which type of material is best showing its heat transfer capabilities.