On the Oxidation Mechanism of n-Dodecane under Pure Oxygen Conditions from Low to High Temperatures

This study investigates the combustion characteristics of n-dodecane under pure oxygen conditions, a critical scenario for rocket propulsion systems. Advanced laser absorption diagnostics were employed to measure the oxidation of key species, including n-dodecane, CO, and H2O, across a wide range of temperatures. The experimental data were used to refine chemical kinetic models by optimizing the rate coefficients of key reactions. The optimized models demonstrated improved predictive accuracy for ignition delay times and species concentration profiles, providing deeper insights into the combustion process. These findings enhance the understanding of n-dodecane combustion and contribute to the development of efficient and environmentally sustainable rocket propulsion technologies. Additionally, the study advances modeling methodologies, offering direct implications for the design of more robust and sustainable rocket engines.