Boeing 747-400 vs. McDonnell Douglas F-4 Phantom II

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Boeing 747-400 versus McDonnell Douglas F-4 Phantom II
70.56 m 231 ft 10 in length 19.2 m 63 ft 0 in
19.3 m 63 ft 4 in height 5.03 m 16 ft 6 in
59.49 m 195 ft 4 in wingspan 11.72 m 38 ft 5 in
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H engines Two General Electric J79s
Around 60,000 to 70,000 pounds thrust per engine 17,900 lbs
Around 240,000 to 280,000 pounds total thrust 35,800 lbs
396,834 kg 875,000 lb MTOW 27,965 kg 61,700 lb
13,492 km 7,285 nmi range 3,031 km 1,636 nm
939 km/h 584 mph cruise speed Mach 2.2 2,717 km/h
Typically accommodates 416 passengers in a three-class layout 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.