Lockheed Martin F-35 Lightning II vs. Max Holste M.H.1521 Broussard

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Lockheed Martin F-35 Lightning II versus Max Holste M.H.1521 Broussard
15.67 m 51 ft 4 in length 10.46 m 34 ft 4 in
4.33 m 14 ft 2 in height 2.74 m 9 ft
10.7 m 35 ft 1 in wingspan 12.86 m 42 ft 2 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1 x Lycoming GSO-480-B1A6 flat-six engine
40,000 lb thrust per engine Approximately 295 hp
40,000 lb total thrust Approximately 295 hp
31,800 kg 70,000 lb MTOW 1,900 kg 4,189 lb
1,380 mi 1,200 nm range 1,030 km 556 nm
520 kt 302 mph cruise speed 145 mph 233 km/h
18,000 pounds of total ordinance capacity 5-7 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.