Lockheed L-1011 TriStar 500 vs. Lockheed Martin F-35 Lightning II

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Lockheed L-1011 TriStar 500 versus Lockheed Martin F-35 Lightning II
50.05 m 164 ft 3 in length 15.67 m 51 ft 4 in
16.87 m 55 ft 4 in height 4.33 m 14 ft 2 in
50.09 m 164 ft 4 in wingspan 10.7 m 35 ft 1 in
3 Rolls-Royce RB211 engines engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
42,000 lbf thrust per engine 40,000 lb
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 40,000 lb
231,330 kg 510,000 lb MTOW 31,800 kg 70,000 lb
11,260 km 6,100 nm range 1,380 mi 1,200 nm
525 knots 972 km/h cruise speed 520 kt 302 mph
Max. 315 passengers (typical 253) 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.