Boeing 787-8 vs. Northrop T-38 Talon

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Boeing 787-8 versus Northrop T-38 Talon
57.0 m 187 ft 0 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
265.1 kN (59600 lbf) for Trent 1000-E, 321.6 kN (72300 lbf) for GEnx-1B70 thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
2 * 265.1 kN (59600 lbf) for Trent 1000-E, 2 * 321.6 kN (72300 lbf) for GEnx-1B70 total thrust 4,100 pounds dry thrust; 5,800 with afterburners
227,930 kg 502,500 lb MTOW 12,093 lb 5,485 kg
13,530 km 7,305 nmi range 1,759 km 950 nm
652 mph 1,050 kph cruise speed 745 kts 1,380 km/h
248 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.