McDonnell-Douglas DC-9-30 vs. Lockheed Martin F-35 Lightning II

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McDonnell-Douglas DC-9-30 versus Lockheed Martin F-35 Lightning II
36.36 m 119 ft 3 in length 15.67 m 51 ft 4 in
8.5 m 27 ft 11 in height 4.33 m 14 ft 2 in
28.44 m 93 ft 4 in wingspan 10.7 m 35 ft 1 in
2x Pratt & Whitney JT8D engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
15,000 pound-force thrust per engine 40,000 lb
30,000 pound-force (2 engines) total thrust 40,000 lb
54,885 kg 121,000 lb MTOW 31,800 kg 70,000 lb
2,632 km 1,422 nm range 1,380 mi 1,200 nm
898 km/h 558 mph cruise speed 520 kt 302 mph
Up to 139 passengers 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.