“…It is required to increase the burning rate and thrust of the propellants to meet the capabilities of precision guidance, long-range strike, and efficient destruction for the weapon system. At present, various solutions for improving the burning rate of solid propellants have been used, such as the application of nano-oxidants, high-energy oxidants, and so on. − The above methods could significantly improve the burning rate and specific impulse of propellants but they also have fatal flaws, such as easy agglomeration and poor safety. Furthermore, nanocatalysts have been a hotspot in propellant formulation due to their excellent properties, such as increasing the burn rate, reducing the burn pressure index and characteristic signal, etc. − As a commonly used oxidant, ammonium perchlorate (AP) directly affects the performance of propellants as its content in many types of propellants up to 60–90%, such as composite propellants, composite modified double base propellants, etc. ,− …”