Douglas DC-8-61 vs. Lockheed Martin F-35 Lightning II

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Douglas DC-8-61 versus Lockheed Martin F-35 Lightning II
57.0 m 187 ft 0 in length 15.67 m 51 ft 4 in
13.1 m 43 ft height 4.33 m 14 ft 2 in
45.24 m 148 ft 5 in wingspan 10.7 m 35 ft 1 in
4x P&W JT3D-3B Turbofan engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
18,000 pound-force thrust per engine 40,000 lb
72,000 pound-force total thrust 40,000 lb
147,400 kg 325,000 lb MTOW 31,800 kg 70,000 lb
3,200 nm 5,926 km range 1,380 mi 1,200 nm
483 knots 282 mph cruise speed 520 kt 302 mph
180 to 220 passengers in a mixed-class seating 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.