Airbus A350-900 vs. Northrop T-38 Talon

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Airbus A350-900 versus Northrop T-38 Talon
66.80 m 219 ft 2 in length 14.1 m 46 ft 4 in
17.05 m 55 ft 11 in height 3.9 m 12 ft 10 in
64.75 m 212 ft 5 in wingspan 7.7 m 25 ft 3 in
2 Rolls-Royce Trent XWB engines Two General Electric J85-GE-5A turbojet engines
84,000 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
168,000 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
283,000 kg 623,900 lb MTOW 12,093 lb 5,485 kg
15,372 km 8,300 nm range 1,759 km 950 nm
888 km/h 552 mph cruise speed 745 kts 1,380 km/h
300-350 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.