Bombardier CRJ900 vs. Lockheed Martin F-35 Lightning II

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Bombardier CRJ900 versus Lockheed Martin F-35 Lightning II
36.2 m 118 ft 11 in length 15.67 m 51 ft 4 in
7.5 m 24 ft 7 in height 4.33 m 14 ft 2 in
24.9 m 81 ft 8 in wingspan 10.7 m 35 ft 1 in
2 Turbofans (fuselage mounted) engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
13,360 pounds force thrust per engine 40,000 lb
26,720 pounds force total thrust 40,000 lb
38,330 kg 84,500 lb MTOW 31,800 kg 70,000 lb
2,871 km 1,550 nm range 1,380 mi 1,200 nm
515 mph 829 km/h cruise speed 520 kt 302 mph
Up to 90 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.