Airbus A350-800 vs. Northrop T-38 Talon

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Airbus A350-800 versus Northrop T-38 Talon
60.54 m 198 ft 7 in length 14.1 m 46 ft 4 in
17.05 m 55 ft 11 in height 3.9 m 12 ft 10 in
64.7 m 212 ft 5 in wingspan 7.7 m 25 ft 3 in
2 Turbofans (wing mounted) engines Two General Electric J85-GE-5A turbojet engines
75,760 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
151,520 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
283,000 kg 623,900 lb MTOW 12,093 lb 5,485 kg
11,708 km 6,319 nm range 1,759 km 950 nm
552 mph 888 km/h cruise speed 745 kts 1,380 km/h
Typically carries 300 to 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.