Lockheed Martin F-35 Lightning II vs. North American BT-9

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Lockheed Martin F-35 Lightning II versus North American BT-9
15.67 m 51 ft 4 in length 8.79 m 28 ft 10 in
4.33 m 14 ft 2 in height 2.82 m 9 ft 3 in
10.7 m 35 ft 1 in wingspan 10.97 m 36 ft
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1 x Wright R-975-3 radial engine
40,000 lb thrust per engine Approximately 440 hp
40,000 lb total thrust Approximately 440 hp
31,800 kg 70,000 lb MTOW 4,300 lb 1,950 kg
1,380 mi 1,200 nm range 917 km 495 nm
520 kt 302 mph cruise speed 150 mph 241 km/h
18,000 pounds of total ordinance capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.