Lockheed P-2 Neptune vs. Max Holste M.H.1521 Broussard

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Lockheed P-2 Neptune versus Max Holste M.H.1521 Broussard
30.17 m 99 ft 0 in length 10.46 m 34 ft 4 in
10.15 m 33 ft 4 in height 2.74 m 9 ft
33.53 m 110 ft wingspan 12.86 m 42 ft 2 in
2 x Wright R-3350 radial engines engines 1 x Lycoming GSO-480-B1A6 flat-six engine
Approximately 3,700 hp thrust per engine Approximately 295 hp
Approximately 7,400 hp total thrust Approximately 295 hp
27,216 kg 60,000 lb MTOW 1,900 kg 4,189 lb
7,885 km 4,259 nm range 1,030 km 556 nm
300 mph 483 km/h cruise speed 145 mph 233 km/h
based on configuration 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.