Airbus A330-200 vs. Northrop T-38 Talon

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Airbus A330-200 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
2 Turbofans engines Two General Electric J85-GE-5A turbojet engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Depends on the engine variant total thrust 4,100 pounds dry thrust; 5,800 with afterburners
251,000 kg 553,400 lb MTOW 12,093 lb 5,485 kg
15,094 km 8,150 nm range 1,759 km 950 nm
531 mph 855 km/h cruise speed 745 kts 1,380 km/h
220-260 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.