COMPARISON OF ABLATION RESISTANCE AND THERMAL THERMAL CONDUCTIVITY OF C-PH AND CNT CNT COMPOSITE LAMINATES

Supersonic aerospace vehicles which operate at very high speeds are supposed to sustain lots of heat due to skin friction. There is always a need for materials which are light in weight and show excellent thermal resistance. The current study compares the thermal conductivity and the ablation resistance of CNT and C-Ph laminates through series of experimental procedures. KEYWORDS: Ablation Resistance, Thermal Conductivity of Composites & C-Ph and CNT