Bombardier CS300 vs. Lockheed Martin F-35 Lightning II

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Bombardier CS300 versus Lockheed Martin F-35 Lightning II
38.0 m 124 ft 7 in length 15.67 m 51 ft 4 in
11.5 m 37 ft 9 in height 4.33 m 14 ft 2 in
35.1 m 115 ft 2 in wingspan 10.7 m 35 ft 1 in
2x Pratt & Whitney PurePower PW1000G engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
93.4 kN thrust per engine 40,000 lb
186.8 kN total thrust 40,000 lb
67,585 kg 149,000 lb MTOW 31,800 kg 70,000 lb
5,463 km 2,952 nm range 1,380 mi 1,200 nm
871 km/h 541 mph cruise speed 520 kt 302 mph
130 to 145 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.