Airbus A220-100 vs. Northrop T-38 Talon

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Airbus A220-100 versus Northrop T-38 Talon
35.0 m 114 ft 10 in length 14.1 m 46 ft 4 in
11.5 m 37 ft 9 in height 3.9 m 12 ft 10 in
35.1 m 115 ft 2 in wingspan 7.7 m 25 ft 3 in
2 Turbofans (wing mounted) engines Two General Electric J85-GE-5A turbojet engines
21,000–23,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
42,000–46,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
63,100 kg 139,100 lb MTOW 12,093 lb 5,485 kg
6,390 km 3,451 nm range 1,759 km 950 nm
871 km/h 541 mph cruise speed 745 kts 1,380 km/h
Typical seating 2-class 100-120 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.