McDonnell-Douglas DC-10-30 vs. Lockheed Martin F-35 Lightning II

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McDonnell-Douglas DC-10-30 versus Lockheed Martin F-35 Lightning II
55.35 m 181 ft 8 in length 15.67 m 51 ft 4 in
17.8 m 58 ft 5 in height 4.33 m 14 ft 2 in
50.39 m 165 ft 4 in wingspan 10.7 m 35 ft 1 in
3x GE CF6-50C Turbofan engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
54,000 lbf thrust per engine 40,000 lb
162,000 lbf total thrust 40,000 lb
251,744 kg 555,000 lb MTOW 31,800 kg 70,000 lb
9,630 km 5,200 nm range 1,380 mi 1,200 nm
507 knots 939 km/h cruise speed 520 kt 302 mph
Up to 380 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.