Airbus A321-200 vs. Northrop T-38 Talon

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Airbus A321-200 versus Northrop T-38 Talon
44.51 m 146 ft 0 in length 14.1 m 46 ft 4 in
11.76 m 38 ft 7 in height 3.9 m 12 ft 10 in
35.8 m 117 ft 5 in wingspan 7.7 m 25 ft 3 in
2 GE CFM56-5B3 engines Two General Electric J85-GE-5A turbojet engines
31,600 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
63,200 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
89,000 kg 196,200 lb MTOW 12,093 lb 5,485 kg
4,000 nmi 7,408 km range 1,759 km 950 nm
871 km/h 541 mph cruise speed 745 kts 1,380 km/h
185 to 220 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.