Airbus A340-600 vs. McDonnell Douglas F-4 Phantom II

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Airbus A340-600 versus McDonnell Douglas F-4 Phantom II
75.36 m 247 ft 3 in length 19.2 m 63 ft 0 in
17.93 m 58 ft 10 in height 5.03 m 16 ft 6 in
63.45 m 208 ft 2 in wingspan 11.72 m 38 ft 5 in
4 x Rolls-Royce Trent 556 engines Two General Electric J79s
56,000 lbs thrust per engine 17,900 lbs
224,000 lbs total thrust 35,800 lbs
380,000 kg 837,800 lb MTOW 27,965 kg 61,700 lb
14,450 km 7,804 nm range 3,031 km 1,636 nm
890 km/h 553 mph cruise speed Mach 2.2 2,717 km/h
320-370 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.