Northrop T-38 Talon vs. Airbus A380-800F

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Northrop T-38 Talon versus Airbus A380-800F
14.1 m 46 ft 4 in length 72.73 m 238 ft 7 in
3.9 m 12 ft 10 in height 24.09 m 79 ft
7.7 m 25 ft 3 in wingspan 79.75 m 261 ft 8 in
Two General Electric J85-GE-5A turbojet engines engines 4 x Engine Alliance GP7200 turbofan engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 280,000 to 320,000 pounds
12,093 lb 5,485 kg MTOW 590,000 kg 1,300,733 lb
1,759 km 950 nm range 14,800 km 7,992 nm
745 kts 1,380 km/h cruise speed 903 km/h 561 mph
Two (student and instructor) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.