Boeing 787-9 vs. Northrop T-38 Talon

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Boeing 787-9 versus Northrop T-38 Talon
63.0 m 206 ft 9 in length 14.1 m 46 ft 4 in
17 m 55 ft 9 in height 3.9 m 12 ft 10 in
60 m 196 ft 1 wingspan 7.7 m 25 ft 3 in
GEnx-1B / Trent 1000 engines Two General Electric J85-GE-5A turbojet engines
76,100 pounds thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
152,200 pounds total thrust 4,100 pounds dry thrust; 5,800 with afterburners
254,000 kg 560,000 lb MTOW 12,093 lb 5,485 kg
14,140 km 7,635 nmi range 1,759 km 950 nm
652 mph 1,050 kph cruise speed 745 kts 1,380 km/h
290 passengers 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.