“…To achieve fast efficiency of propellant oxidizers additives are added to improve its decomposition process, which is easily prepared, easily separable, and environmentally friendly. [1][2][3][4] Research in the field of thermolysis of propellant oxidizers, namely ammonium perchlorate (AP), 3-nitro-2,4-dihydro-3H-1,2,4-triazol-5-one (NTO), ammonium nitrate (AN), 1,3,5,7-tetranitro-1,3,5,7-tetrazocane (HMX), 1,3,5-trinitroperhydro-1,3,5-triazine (RDX), and hexanitrohexaazaisowurtzitane (CL-20), is capturing increasing interest from decades to the present day for the enhancement of their decomposition performance, thermal stability, detonation properties, thermal sensitivity, and toxicity. 3,[5][6][7][8][9] Among these oxidants, AN is the widely used oxidizing agent due to its low-temperature and chlorine-free decomposition, which can replace AP-based propulsion systems.…”