Airbus A380-800 vs. Northrop T-38 Talon

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Airbus A380-800 versus Northrop T-38 Talon
72.72 m 238 ft 7 in length 14.1 m 46 ft 4 in
24.09 m 79 ft height 3.9 m 12 ft 10 in
79.75 m 261 ft 8 in wingspan 7.7 m 25 ft 3 in
4 engines Two General Electric J85-GE-5A turbojet engines
70000lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
280000lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
560,000 kg 1,234,600 lb MTOW 12,093 lb 5,485 kg
14,800 km 8,000 nm range 1,759 km 950 nm
1,050 km/h 652 mph cruise speed 745 kts 1,380 km/h
525-853 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.