Airbus A321-200 vs. McDonnell Douglas F-4 Phantom II

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Airbus A321-200 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
2 GE CFM56-5B3 engines Two General Electric J79s
31,600 lbs thrust per engine 17,900 lbs
63,200 lbs total thrust 35,800 lbs
89,000 kg 196,200 lb MTOW 27,965 kg 61,700 lb
4,000 nmi 7,408 km range 3,031 km 1,636 nm
871 km/h 541 mph cruise speed Mach 2.2 2,717 km/h
185 to 220 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.