Airbus A319 vs. Northrop T-38 Talon

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Airbus A319 versus Northrop T-38 Talon
33.84 m 111 ft 0 in length 14.1 m 46 ft 4 in
11.76 m 38 ft 7 in height 3.9 m 12 ft 10 in
35.8 m 117 ft 5 in wingspan 7.7 m 25 ft 3 in
2 (International Aero Engines V2524-A5) engines Two General Electric J85-GE-5A turbojet engines
27,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
54,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
75,500 kg 166,400 lb MTOW 12,093 lb 5,485 kg
3,700 nmi 6,852 km range 1,759 km 950 nm
829 km/h 515 mph cruise speed 745 kts 1,380 km/h
124 to 156 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.