Boeing 777-8 vs. Northrop T-38 Talon

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Boeing 777-8 versus Northrop T-38 Talon
69.8 m 229 ft 1 in length 14.1 m 46 ft 4 in
19.5 m 64 ft height 3.9 m 12 ft 10 in
71.8 m 235 ft 6 in wingspan 7.7 m 25 ft 3 in
2 x GE9X-105B1A engines Two General Electric J85-GE-5A turbojet engines
105,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
210,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
351,500 kg 775,000 lb MTOW 12,093 lb 5,485 kg
16,000 km 8,638 nm range 1,759 km 950 nm
900 km/h 559 mph cruise speed 745 kts 1,380 km/h
365 (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.