Airbus A340-300X vs. McDonnell Douglas F-4 Phantom II

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Airbus A340-300X versus McDonnell Douglas F-4 Phantom II
63.60 m 208 ft 6 in length 19.2 m 63 ft 0 in
16.7 m 54 ft 9 in height 5.03 m 16 ft 6 in
60.3 m 197 ft 9 in wingspan 11.72 m 38 ft 5 in
4 Turbofan Engines engines Two General Electric J79s
151.2 kN thrust per engine 17,900 lbs
604.8 kN total thrust 35,800 lbs
275,000 kg 606,300 lb MTOW 27,965 kg 61,700 lb
13,699 km 7,403 nm range 3,031 km 1,636 nm
915 km/h 569 mph cruise speed Mach 2.2 2,717 km/h
295 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.