Airbus A321XLR vs. Northrop T-38 Talon

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines Two General Electric J85-GE-5A turbojet engines
33,000 lbs (147 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
66,000 lbs (294 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
101,000 kg 222,700 lb MTOW 12,093 lb 5,485 kg
4,700 nmi 8,704 km range 1,759 km 950 nm
963km/h 598mph cruise speed 745 kts 1,380 km/h
180-220 seats (typical 2-class seating) 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.