Airbus A318 vs. Northrop T-38 Talon

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Airbus A318 versus Northrop T-38 Talon
31.44 m 103 ft 2 in length 14.1 m 46 ft 4 in
12.56 m 41 ft 3 in height 3.9 m 12 ft 10 in
34.1 m 111 ft 11 in wingspan 7.7 m 25 ft 3 in
2x CFM56-5B or 2x PW6000 engines Two General Electric J85-GE-5A turbojet engines
23,300 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
46,600 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
59,000 kg 130,000 lb MTOW 12,093 lb 5,485 kg
5,750 km 3,106 nm range 1,759 km 950 nm
963km/h 598mph cruise speed 745 kts 1,380 km/h
107 to 132 passengers capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.