Airbus A321neo vs. Northrop T-38 Talon

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Airbus A321neo 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines Two General Electric J85-GE-5A turbojet engines
35,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
70,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
97,000 kg 213,800 lb MTOW 12,093 lb 5,485 kg
7,400 km 4,000 nm range 1,759 km 950 nm
828 km/h 514 mph cruise speed 745 kts 1,380 km/h
180 to 220 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.