Airbus A320neo vs. McDonnell Douglas F-4 Phantom II

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Airbus A320neo versus McDonnell Douglas F-4 Phantom II
37.57 m 123 ft 3 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 x PW 1100G or 2 x CFM LEAP-1A engines Two General Electric J79s
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 17,900 lbs
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 35,800 lbs
79,000 kg 174,200 lb MTOW 27,965 kg 61,700 lb
6,300 km 3,403 nm range 3,031 km 1,636 nm
M0.82 101,3 km/h cruise speed Mach 2.2 2,717 km/h
150-180 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.