In this study, we propose a revised coupled combustion model for ammonium perchlorate (AP), leveraging recent advances in the modelling of ammonia and NOx chemistry. A coupled combustion model relies on three founding bricks: a detailed gas-phase kinetic model, a condensed-phase decomposition model, and a pyrolysis law describing the relationship between the surface temperature and mass ow. The proposed gas-phase kinetic model, is validated against data on species sampling in jet-stirred reactors, laminar ame speed, and ignition delay time. These test cases, rarely used by the solid propellant community, highlight deciencies in a reference mechanism from the literature. A new model for AP decomposition in the condensed phase is proposed to be used with the gas-phase mechanism. A suitable pyrolysis law is designed using the Zel'dovich-Novozhilov theory to ensure the stability of the coupled combustion model. The methodology employed is described in detail, for others to replicate. Finally, the overall model is applied to simulate the AP laminar ame in a 1D coupled approach. These calculations provide results on the regression rate, surface temperature, temperature sensitivity and species proles for prescribed initial temperature of AP and ambient pressure. The behavior of the proposed combustion model is presented in comparison with other reference models. The role of gas-phase kinetics in modeling AP combustion is discussed.