“…In addition, fiber‐reinforced, high‐temperature, polymer‐matrix composites are particularly attractive for aerospace structures because of their low density [2, 3], high mechanical strength [2, 4–10], high modulus [2, 4, 6, 8, 9], thermo‐oxidative stability [2, 4, 9, 11, 12], electrical properties [2, 6, 10, 13], and excellent chemical resistance [2, 5, 6, 14]. Various polyimide‐based composites have been studied for use in aerospace applications for these reasons [2, 4, 6, 11, 15]. Phenylethynyl‐endcapped fluorinated polyimides are especially useful because of their environmental stability and high glass‐transition temperature ( T g ) (435–455°C) [8].…”