Max Holste M.H.1521 Broussard vs. Lockheed Martin C-130J Super Hercules

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Max Holste M.H.1521 Broussard versus Lockheed Martin C-130J Super Hercules
10.46 m 34 ft 4 in length 34.37 m 112 ft 9 in
2.74 m 9 ft height 11.86 m 38 ft 11 in
12.86 m 42 ft 2 in wingspan 40.41 m 132 ft 7 in
1 x Lycoming GSO-480-B1A6 flat-six engine engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 295 hp thrust per engine Approximately 4,700 hp per engine
Approximately 295 hp total thrust Approximately 18,800 hp total
1,900 kg 4,189 lb MTOW 76,610 kg 168,900 lb
1,030 km 556 nm range 4,600 km 2,485 nm
145 mph 233 km/h cruise speed 660 km/h 410 mph
5-7 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.