Airbus A320-200 vs. McDonnell Douglas F-4 Phantom II

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Airbus A320-200 versus McDonnell Douglas F-4 Phantom II
38.7 m 127 ft 0 in length 19.2 m 63 ft 0 in
17.4 m 57 ft 1 in height 5.03 m 16 ft 6 in
35.8 m 117 ft 5 in wingspan 11.72 m 38 ft 5 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines Two General Electric J79s
Between 21,000 - 33,000 lbf thrust per engine 17,900 lbs
Between 42,000 - 66,000 lbf total thrust 35,800 lbs
77,000 kg 169,800 lb MTOW 27,965 kg 61,700 lb
5,700 km 3,078 nm range 3,031 km 1,636 nm
530 mph 853 km/h cruise speed Mach 2.2 2,717 km/h
Typically between 140-180 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.