Airbus A350-900ULR vs. McDonnell Douglas F-4 Phantom II

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Airbus A350-900ULR versus McDonnell Douglas F-4 Phantom II
66.80 m 219 ft 2 in length 19.2 m 63 ft 0 in
17.05 m 55 ft 11 in height 5.03 m 16 ft 6 in
64.75 m 212 ft 5 in wingspan 11.72 m 38 ft 5 in
2 Rolls-Royce Trent XWB engines Two General Electric J79s
84,000 lbs thrust per engine 17,900 lbs
168,000 lbs total thrust 35,800 lbs
280,000 kg 617,300 lb MTOW 27,965 kg 61,700 lb
17,964 km 9,700 nm range 3,031 km 1,636 nm
552 mph 888 km/h cruise speed Mach 2.2 2,717 km/h
300-350 passengers in three classes 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.