Boeing 777-200 vs. Northrop T-38 Talon

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Boeing 777-200 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
General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 engines Two General Electric J85-GE-5A turbojet engines
Up to 94,000 pounds thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Up to 188,000 pounds total thrust 4,100 pounds dry thrust; 5,800 with afterburners
299,370 kg 660,000 lb MTOW 12,093 lb 5,485 kg
5,240 nm 9,711 km range 1,759 km 950 nm
560 mph 901 km/h cruise speed 745 kts 1,380 km/h
305 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.