Lockheed Martin C-130J Super Hercules vs. Bell 412

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Lockheed Martin C-130J Super Hercules versus Bell 412
34.37 m 112 ft 9 in length 17,10 m 56 ft 1 in
11.86 m 38 ft 11 in height 3,48 m 11 ft 5 in
40.41 m 132 ft 7 in wingspan
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
Approximately 4,700 hp per engine thrust per engine 1,800 hp
Approximately 18,800 hp total total thrust 3,600 hp
76,610 kg 168,900 lb MTOW 5,400 kg 11,905 lb
4,600 km 2,485 nm range 659 km 356 nm
660 km/h 410 mph cruise speed 259 km/h 161 mph
based on configuration capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.