Bombardier CRJ700 vs. Lockheed Martin F-35 Lightning II

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Bombardier CRJ700 versus Lockheed Martin F-35 Lightning II
32.51 m 106 ft 8 in length 15.67 m 51 ft 4 in
7.6 m 24 ft 11 in height 4.33 m 14 ft 2 in
23.24 m 76 ft 3 in wingspan 10.7 m 35 ft 1 in
2 x General Electric CF34-8C5B1 turbofans engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
13,790 pounds (61.3 kN) thrust per engine 40,000 lb
27,580 pounds (122.6 kN) total thrust 40,000 lb
33,113 kg 73,000 lb MTOW 31,800 kg 70,000 lb
2,655 km 1,434 nm range 1,380 mi 1,200 nm
514 mph 828 km/h cruise speed 520 kt 302 mph
Up to 78 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.