Analysis Of Carbon Nano Particle Variant As The Propellant Fuel To Increase Specific Impulses Of Rockets

This study uses coal and coconut shell nanocarbon variant fuels to compare the precise thrust and impulse parameters of various propellant fuels. The key factors affecting rocket performance are specific impulses and impulses. The fuel type, material composition, heat flow, and burning period characteristics all affect the precise thrust and impulses. It has been demonstrated that nanocarbon has valuable properties and a lengthy combustion time.