Airbus A310-300 vs. Northrop T-38 Talon

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Airbus A310-300 versus Northrop T-38 Talon
46.66 m 153 ft 1 in length 14.1 m 46 ft 4 in
15.8 m 51 ft 10 in height 3.9 m 12 ft 10 in
43.9 m 144 ft wingspan 7.7 m 25 ft 3 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Two General Electric J85-GE-5A turbojet engines
52,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
104,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
148,768 kg 328,000 lb MTOW 12,093 lb 5,485 kg
8,050 km 4,348 nm range 1,759 km 950 nm
482 knots 279 mph cruise speed 745 kts 1,380 km/h
190-230 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.