“…Composite solid propellants (CSPs), composed of oxidants, additives, binder, and fuels, are power producers widely used in aviation, space flight, and missiles. , Among these ingredients, oxidants usually occupy more than a half of CSPs and greatly affect the performance of CSPs. Ammonium perchlorate (AP) is a common oxidant in CSPs, , and its thermal decomposition properties can greatly influence the combustion performance of CSPs. , It is reported that AP-based CSPs can display a high specific impulse, low-pressure exponent, and fast burning rate by increasing the heat release and decreasing the decomposition temperature of AP. − Therefore, promoting the thermal decomposition of AP can enhance the combustion performance of CSPs.…”