Airbus A330-900neo vs. McDonnell Douglas F-4 Phantom II

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Airbus A330-900neo versus McDonnell Douglas F-4 Phantom II
63.66 m 208 ft 10 in length 19.2 m 63 ft 0 in
16.79 m 55 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 pound-force thrust per engine 17,900 lbs
144,000 lbf total thrust 35,800 lbs
251,000 kg 553,400 lb MTOW 27,965 kg 61,700 lb
7,200 nm 13,334 km range 3,031 km 1,636 nm
496 knots 919 km/h cruise speed Mach 2.2 2,717 km/h
260-300 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.