Airbus A340-500 vs. Northrop T-38 Talon

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Airbus A340-500 versus Northrop T-38 Talon
67.93 m 222 ft 10 in length 14.1 m 46 ft 4 in
17.53 m 57 ft 6 in height 3.9 m 12 ft 10 in
63.45 m 208 ft 2 in wingspan 7.7 m 25 ft 3 in
4 Rolls-Royce Trent 500 engines Two General Electric J85-GE-5A turbojet engines
54,000 lbf (240 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
216,000 lbf (960 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
380,000 kg 837,800 lb MTOW 12,093 lb 5,485 kg
16,670 km 9,000 nm range 1,759 km 950 nm
475 knots 880 km/h cruise speed 745 kts 1,380 km/h
Typical seating 3-class 270-310 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.