Research Progress of Burning Rate Inhibitors in Solid Heterogeneous Propellants

Abstract The advancement of solid rocket technology has increased demand for high‐performing propellants, particularly in the aerospace industry. Solid propellants are an essential component of rocket engines, and their stable combustion and adjustable burning rate throughout a wide pressure range significantly affect the performance of motors. The burning rate modifiers include catalysts and inhibitors. Solid rocket motors for different purposes require propellants with different burning rates. Using propellants that burn at a slower rate is beneficial for the smooth release of propellant energy, reducing the loss of energy in the process of high burning rate release and improving the endurance time of missile engines. Therefore, it is necessary to decrease the burning rate of propellant. This article summarizes the development of burning rate inhibitors (BRIs) and analyzes the mechanisms and behaviors of different BRIs, including amide‐based compounds, metal salts, and cationic surfactants, that affect the combustion of propellants.