Lockheed Martin F-35 Lightning II vs. North American Rockwell OV-10 Bronco

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Lockheed Martin F-35 Lightning II versus North American Rockwell OV-10 Bronco
15.67 m 51 ft 4 in length 12.7 m 41 ft 7 in
4.33 m 14 ft 2 in height 4.62 m 15 ft 2 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 2 x Garrett T76-G-420/421 turboprop engines
40,000 lb thrust per engine Approximately 715 hp each
40,000 lb total thrust Approximately 1,430 hp total
31,800 kg 70,000 lb MTOW 14,444 lb 6,553 kg
1,380 mi 1,200 nm range 1,931 km 1,043 nm
520 kt 302 mph cruise speed 244 mph 393 km/h
18,000 pounds of total ordinance capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.