Airbus A321neo vs. McDonnell Douglas F-4 Phantom II

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Airbus A321neo 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines Two General Electric J79s
35,000 lb thrust per engine 17,900 lbs
70,000 lb total thrust 35,800 lbs
97,000 kg 213,800 lb MTOW 27,965 kg 61,700 lb
7,400 km 4,000 nm range 3,031 km 1,636 nm
828 km/h 514 mph cruise speed Mach 2.2 2,717 km/h
180 to 220 passengers 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.