Airbus A340-300X vs. Northrop T-38 Talon

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Airbus A340-300X versus Northrop T-38 Talon
63.60 m 208 ft 6 in length 14.1 m 46 ft 4 in
16.7 m 54 ft 9 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 Turbofan Engines engines Two General Electric J85-GE-5A turbojet engines
151.2 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
604.8 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
275,000 kg 606,300 lb MTOW 12,093 lb 5,485 kg
13,699 km 7,403 nm range 1,759 km 950 nm
915 km/h 569 mph cruise speed 745 kts 1,380 km/h
295 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.