Bombardier CS100 vs. Lockheed Martin F-35 Lightning II

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Bombardier CS100 versus Lockheed Martin F-35 Lightning II
35.00 m 114 ft 10 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
2 x Pratt & Whitney PurePower PW1500G engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
84.1 kN thrust per engine 40,000 lb
168.2 kN total thrust 40,000 lb
54,931 kg 121,100 lb MTOW 31,800 kg 70,000 lb
4,074 km 2,200 nm range 1,380 mi 1,200 nm
871 km/h 541 mph cruise speed 520 kt 302 mph
110 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.