Airbus A321XLR vs. McDonnell Douglas F-4 Phantom II

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Airbus A321XLR versus McDonnell Douglas F-4 Phantom II
44.51 m 146 ft 0 in length 19.2 m 63 ft 0 in
11.76 m 38 ft 7 in height 5.03 m 16 ft 6 in
35.8 m 117 ft 5 in wingspan 11.72 m 38 ft 5 in
CFM LEAP-1A and P&W PW1100G engines Two General Electric J79s
33,000 lbs (147 kN) thrust per engine 17,900 lbs
66,000 lbs (294 kN) total thrust 35,800 lbs
101,000 kg 222,700 lb MTOW 27,965 kg 61,700 lb
4,700 nmi 8,704 km range 3,031 km 1,636 nm
963km/h 598mph cruise speed Mach 2.2 2,717 km/h
180-220 seats (typical 2-class seating) capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.