Airbus A320-200 vs. Northrop T-38 Talon

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Airbus A320-200 versus Northrop T-38 Talon
38.7 m 127 ft 0 in length 14.1 m 46 ft 4 in
17.4 m 57 ft 1 in height 3.9 m 12 ft 10 in
35.8 m 117 ft 5 in wingspan 7.7 m 25 ft 3 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines Two General Electric J85-GE-5A turbojet engines
Between 21,000 - 33,000 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Between 42,000 - 66,000 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
77,000 kg 169,800 lb MTOW 12,093 lb 5,485 kg
5,700 km 3,078 nm range 1,759 km 950 nm
530 mph 853 km/h cruise speed 745 kts 1,380 km/h
Typically between 140-180 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.