Airbus A330-800neo vs. Northrop T-38 Talon

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Airbus A330-800neo versus Northrop T-38 Talon
58.82 m 193 ft 0 in length 14.1 m 46 ft 4 in
17.39 m 57 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 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
145,668 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
251,000 kg 553,400 lb MTOW 12,093 lb 5,485 kg
8,150 nm 15,094 km range 1,759 km 950 nm
496 knots 919 km/h cruise speed 745 kts 1,380 km/h
220-260 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.