Airbus A340-200 vs. Northrop T-38 Talon

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Airbus A340-200 versus Northrop T-38 Talon
59.4 m 194 ft 11 in length 14.1 m 46 ft 4 in
16.8 m 55 ft 1 in height 3.9 m 12 ft 10 in
60.3 m 197 ft 9 in wingspan 7.7 m 25 ft 3 in
4 x CFM International CFM56-5C4 engines Two General Electric J85-GE-5A turbojet engines
34,000 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
136,000 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
275,000 kg 606,300 lb MTOW 12,093 lb 5,485 kg
12,400 km 6,699 nm range 1,759 km 950 nm
880 km/h 547 mph cruise speed 745 kts 1,380 km/h
Typical seating 3-class 210-250 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.