Boeing 777-200LR Worldliner vs. Northrop T-38 Talon

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Boeing 777-200LR Worldliner versus Northrop T-38 Talon
63.7 m 209 ft 1 in length 14.1 m 46 ft 4 in
18.6 m 61 ft height 3.9 m 12 ft 10 in
64.8 m 212 ft 7 in wingspan 7.7 m 25 ft 3 in
2 x GE90-115B engines Two General Electric J85-GE-5A turbojet engines
115,300 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
230,600 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
347,500 kg 766,100 lb MTOW 12,093 lb 5,485 kg
15,843 km 8,555 nmi range 1,759 km 950 nm
950 km/h 590 mph cruise speed 745 kts 1,380 km/h
317 (2-class) 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.