“…During service, aircraft structures are subjected to dynamic loads such as impact with foreign bodies, projectile impacts, and shock waves, which may significantly affect the mechanical properties of thermoplastic fiber-reinforced (TFR) composite materials used for these high-performance structures [1][2][3]. Thus, a reliable design of the composite components requires a detailed mechanical characterization at high strain rates because in most cases, due to the lack of dynamic properties, static properties are used in material selection and design, which can result in excessive structural weight or cause unexplained and untimely failure [1,[4][5][6].…”