Airbus A330-900neo vs. Northrop T-38 Talon

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Airbus A330-900neo versus Northrop T-38 Talon
63.66 m 208 ft 10 in length 14.1 m 46 ft 4 in
16.79 m 55 ft 1 in height 3.9 m 12 ft 10 in
64 m 210 ft wingspan 7.7 m 25 ft 3 in
2x Rolls-Royce Trent 7000-72 Turbofan engines Two General Electric J85-GE-5A turbojet engines
72,834 pound-force thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
144,000 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
251,000 kg 553,400 lb MTOW 12,093 lb 5,485 kg
7,200 nm 13,334 km range 1,759 km 950 nm
496 knots 919 km/h cruise speed 745 kts 1,380 km/h
260-300 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.