Boeing 777-300ER vs. Northrop T-38 Talon

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Boeing 777-300ER versus Northrop T-38 Talon
73.9 m 242 ft 4 in length 14.1 m 46 ft 4 in
18.5 m 60 ft 8 in height 3.9 m 12 ft 10 in
64.8 m 212 ft 7 in wingspan 7.7 m 25 ft 3 in
GE90-115BL engines Two General Electric J85-GE-5A turbojet engines
115,300 lbf (513 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
230,600 lbf (1026 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
351,534 kg 775,000 lb MTOW 12,093 lb 5,485 kg
13,649 km 7,370 nmi range 1,759 km 950 nm
510 knots 945 km/h cruise speed 745 kts 1,380 km/h
396 passengers (2-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.