Airbus A350-900ULR vs. Northrop T-38 Talon

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Airbus A350-900ULR 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
280,000 kg 617,300 lb MTOW 12,093 lb 5,485 kg
17,964 km 9,700 nm range 1,759 km 950 nm
552 mph 888 km/h cruise speed 745 kts 1,380 km/h
300-350 passengers in three classes 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.