Airbus A350-800 vs. McDonnell Douglas F-4 Phantom II

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Airbus A350-800 versus McDonnell Douglas F-4 Phantom II
60.54 m 198 ft 7 in length 19.2 m 63 ft 0 in
17.05 m 55 ft 11 in height 5.03 m 16 ft 6 in
64.7 m 212 ft 5 in wingspan 11.72 m 38 ft 5 in
2 Turbofans (wing mounted) engines Two General Electric J79s
75,760 lb thrust per engine 17,900 lbs
151,520 lb total thrust 35,800 lbs
283,000 kg 623,900 lb MTOW 27,965 kg 61,700 lb
11,708 km 6,319 nm range 3,031 km 1,636 nm
552 mph 888 km/h cruise speed Mach 2.2 2,717 km/h
Typically carries 300 to 350 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.