Boeing 747-8I vs. McDonnell Douglas F-4 Phantom II

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Boeing 747-8I versus McDonnell Douglas F-4 Phantom II
76.25 m 250 ft 2 in length 19.2 m 63 ft 0 in
19.35 m 63 ft 6 in height 5.03 m 16 ft 6 in
68.45 m 224 ft 7 in wingspan 11.72 m 38 ft 5 in
4x General Electric GEnx 2B67 Turbofan engines Two General Electric J79s
66,500 pounds thrust per engine 17,900 lbs
266,000 pounds total thrust 35,800 lbs
443,613 kg 977,500 lb MTOW 27,965 kg 61,700 lb
8,000 nm 14,816 km range 3,031 km 1,636 nm
Mach 0.86 1,062 km/h cruise speed Mach 2.2 2,717 km/h
467 passengers (three-class configuration) 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.