Airbus A319neo vs. Northrop T-38 Talon

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Airbus A319neo 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 x PW 1100G or 2 x CFM LEAP-1A engines Two General Electric J85-GE-5A turbojet engines
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
75,500 kg 166,400 lb MTOW 12,093 lb 5,485 kg
6,850 km 3,702 nm range 1,759 km 950 nm
530 mph 853 km/h cruise speed 745 kts 1,380 km/h
120-150 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.