Lockheed Martin F-35 Lightning II vs. Percival Provost

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Lockheed Martin F-35 Lightning II versus Percival Provost
15.67 m 51 ft 4 in length 9.0 m 29 ft 6 in
4.33 m 14 ft 2 in height 3.02 m 9 ft 11 in
10.7 m 35 ft 1 in wingspan 12.19 m 40 ft
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1 x Alvis Leonides Major 755/1 inline engine
40,000 lb thrust per engine Approximately 550 hp
40,000 lb total thrust Approximately 550 hp
31,800 kg 70,000 lb MTOW 5,500 lb 2,495 kg
1,380 mi 1,200 nm range 1,127 km 608 nm
520 kt 302 mph cruise speed 175 mph 282 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.