Airbus A300-600 vs. Northrop T-38 Talon

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Airbus A300-600 versus Northrop T-38 Talon
54.10 m 177 ft 6 in length 14.1 m 46 ft 4 in
16.5 m 54 ft 2 in height 3.9 m 12 ft 10 in
44.84 m 147 ft 1 in wingspan 7.7 m 25 ft 3 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Two General Electric J85-GE-5A turbojet engines
56,000lb to 61,500lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
112,000–123,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
171,700 kg 378,600 lb MTOW 12,093 lb 5,485 kg
7,500 km 4,052 nm range 1,759 km 950 nm
897 km/h 557 mph cruise speed 745 kts 1,380 km/h
210-250 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.