Bombardier CRJ1000 vs. Lockheed Martin F-35 Lightning II

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Bombardier CRJ1000 versus Lockheed Martin F-35 Lightning II
39.1 m 128 ft 5 in length 15.67 m 51 ft 4 in
7.5 m 24 ft 7 in height 4.33 m 14 ft 2 in
26.2 m 86 ft wingspan 10.7 m 35 ft 1 in
2 GE CF34-8C5A1 turbofans engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 40,000 lb
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 40,000 lb
41,640 kg 91,800 lb MTOW 31,800 kg 70,000 lb
3,004 km 1,623 nm range 1,380 mi 1,200 nm
515 mph 829 km/h cruise speed 520 kt 302 mph
100 (common) 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.