Airbus A330-300 vs. Northrop T-38 Talon

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Airbus A330-300 versus Northrop T-38 Talon
63.66 m 208 ft 9 in length 14.1 m 46 ft 4 in
16.79 m 55 ft 1 in height 3.9 m 12 ft 10 in
60.3 m 197 ft 9 in wingspan 7.7 m 25 ft 3 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines Two General Electric J85-GE-5A turbojet engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Depends on the engine type total thrust 4,100 pounds dry thrust; 5,800 with afterburners
242,000 kg 533,600 lb MTOW 12,093 lb 5,485 kg
11,750 km 6,346 nm range 1,759 km 950 nm
900 km/h 559 mph cruise speed 745 kts 1,380 km/h
250-290 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.