The study of the combustion property of newly designed propellant by means of computational simulation is an e cient pathway for assessment and could avoid exposure to hazardous chemicals. An RDX modi ed triple-base solid propellant formula was proposed in this study. Reactive molecular dynamics simulations employing ReaxFF-lg force eld were performed to explore the thermal decomposition property of the propellant for a variety of temperatures. The reaction kinetics of the system and major ingredients were analyzed and the apparent decomposition activation energies were calculated. The population of decomposition intermediates and products is thoroughly investigated. H2O is consumed at high temperatures indicating a water-gas reaction that could reduce carbon clusters during the combustion of solid propellant. The water-gas reaction, as well as the population of H 2 at high temperature, point out the way of adjusting the formula of the propellant, that is adds fuel and oxidizer to improve combustion temperature and oxygen balance.