Airbus A350-1000 vs. Northrop T-38 Talon

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Airbus A350-1000 versus Northrop T-38 Talon
73.79 m 242 ft 1 in length 14.1 m 46 ft 4 in
17.08 m 56 ft height 3.9 m 12 ft 10 in
64.75 m 212 ft 5 in wingspan 7.7 m 25 ft 3 in
2 Trent XWB-97 turbofan engines engines Two General Electric J85-GE-5A turbojet engines
97,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
194,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
319,000 kg 703,300 lb MTOW 12,093 lb 5,485 kg
16,100 km 8,695 nm range 1,759 km 950 nm
1,099 km/h 683 mph cruise speed 745 kts 1,380 km/h
350 to 410 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.