Airbus A330-200 vs. McDonnell Douglas F-4 Phantom II

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Airbus A330-200 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
2 Turbofans engines Two General Electric J79s
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 17,900 lbs
Depends on the engine variant total thrust 35,800 lbs
251,000 kg 553,400 lb MTOW 27,965 kg 61,700 lb
15,094 km 8,150 nm range 3,031 km 1,636 nm
531 mph 855 km/h cruise speed Mach 2.2 2,717 km/h
220-260 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.