Boeing 747-8I vs. Northrop T-38 Talon

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Boeing 747-8I versus Northrop T-38 Talon
76.25 m 250 ft 2 in length 14.1 m 46 ft 4 in
19.35 m 63 ft 6 in height 3.9 m 12 ft 10 in
68.45 m 224 ft 7 in wingspan 7.7 m 25 ft 3 in
4x General Electric GEnx 2B67 Turbofan engines Two General Electric J85-GE-5A turbojet engines
66,500 pounds thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
266,000 pounds total thrust 4,100 pounds dry thrust; 5,800 with afterburners
443,613 kg 977,500 lb MTOW 12,093 lb 5,485 kg
8,000 nm 14,816 km range 1,759 km 950 nm
Mach 0.86 1,062 km/h cruise speed 745 kts 1,380 km/h
467 passengers (three-class configuration) 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.