Consolidated B-24 Liberator vs. McDonnell Douglas F-4 Phantom II

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Consolidated B-24 Liberator versus McDonnell Douglas F-4 Phantom II
20.42 m 67 ft 0 in length 19.2 m 63 ft 0 in
5.49 m 18 ft height 5.03 m 16 ft 6 in
33.53 m 110 ft wingspan 11.72 m 38 ft 5 in
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines Two General Electric J79s
1,200 hp, 1,200 hp each thrust per engine 17,900 lbs
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust 35,800 lbs
26,580 kg 58,600 lb MTOW 27,965 kg 61,700 lb
2,850 mi 2,481 nm range 3,031 km 1,636 nm
175 mph 282 km/h cruise speed Mach 2.2 2,717 km/h
8,000 pounds 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.