Consolidated B-24 Liberator vs. Lockheed Martin F-35 Lightning II

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Consolidated B-24 Liberator versus Lockheed Martin F-35 Lightning II
20.42 m 67 ft 0 in length 15.67 m 51 ft 4 in
5.49 m 18 ft height 4.33 m 14 ft 2 in
33.53 m 110 ft wingspan 10.7 m 35 ft 1 in
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
1,200 hp, 1,200 hp each thrust per engine 40,000 lb
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust 40,000 lb
26,580 kg 58,600 lb MTOW 31,800 kg 70,000 lb
2,850 mi 2,481 nm range 1,380 mi 1,200 nm
175 mph 282 km/h cruise speed 520 kt 302 mph
8,000 pounds capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.