Boeing 717-200HGW vs. Lockheed Martin F-35 Lightning II

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Boeing 717-200HGW versus Lockheed Martin F-35 Lightning II
37.80 m 123 ft 11 in length 15.67 m 51 ft 4 in
8.87 m 29 ft 1 in height 4.33 m 14 ft 2 in
28.44 m 93 ft 4 in wingspan 10.7 m 35 ft 1 in
2 Rolls-Royce BR715 engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine 40,000 lb
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust 40,000 lb
54,885 kg 121,000 lb MTOW 31,800 kg 70,000 lb
2,060 nm 3,814 km range 1,380 mi 1,200 nm
811 km/h 504 mph cruise speed 520 kt 302 mph
106 passengers in a 2 class configuration 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.