Lockheed U-2 vs. Max Holste M.H.1521 Broussard

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Lockheed U-2 versus Max Holste M.H.1521 Broussard
19.2 m 63 ft 0 in length 10.46 m 34 ft 4 in
4.8 m 15 ft 9 in height 2.74 m 9 ft
32 m 105 ft wingspan 12.86 m 42 ft 2 in
1 × General Electric F118-101 engines 1 x Lycoming GSO-480-B1A6 flat-six engine
17,000 lbf (76 kN) thrust per engine Approximately 295 hp
17,000 lbf (76 kN) total thrust Approximately 295 hp
18,144 kg 40,000 lb MTOW 1,900 kg 4,189 lb
6,090 nm 11,278 km range 1,030 km 556 nm
475 mph 764 km/h cruise speed 145 mph 233 km/h
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.