Airbus A330-800neo vs. McDonnell Douglas F-4 Phantom II

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Airbus A330-800neo versus McDonnell Douglas F-4 Phantom II
58.82 m 193 ft 0 in length 19.2 m 63 ft 0 in
17.39 m 57 ft 1 in height 5.03 m 16 ft 6 in
64 m 210 ft wingspan 11.72 m 38 ft 5 in
2x Rolls-Royce Trent 7000-72 Turbofan engines Two General Electric J79s
72,834 lb thrust per engine 17,900 lbs
145,668 lb total thrust 35,800 lbs
251,000 kg 553,400 lb MTOW 27,965 kg 61,700 lb
8,150 nm 15,094 km range 3,031 km 1,636 nm
496 knots 919 km/h cruise speed Mach 2.2 2,717 km/h
220-260 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.