Boeing 777-9 vs. Northrop T-38 Talon

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Boeing 777-9 versus Northrop T-38 Talon
76.72 m 251 ft 9 in length 14.1 m 46 ft 4 in
19.65 m 64 ft 6 in height 3.9 m 12 ft 10 in
71.75 m 235 ft 5 in wingspan 7.7 m 25 ft 3 in
GE9X engines Two General Electric J85-GE-5A turbojet engines
105,000 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
210,000 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
351,550 kg 775,000 lb MTOW 12,093 lb 5,485 kg
13,500 km 7,285 nmi range 1,759 km 950 nm
590 mph 950 km/h cruise speed 745 kts 1,380 km/h
426 (Typical 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.