Mitsubishi A6M Zero vs. Lockheed Martin C-130J Super Hercules

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Mitsubishi A6M Zero versus Lockheed Martin C-130J Super Hercules
9.06 m 29 ft 9 in length 34.37 m 112 ft 9 in
3.05 m 10 ft height 11.86 m 38 ft 11 in
12 m 39 ft 4 in wingspan 40.41 m 132 ft 7 in
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine engines 4 x Rolls-Royce AE 2100D3 turboprop engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine Approximately 4,700 hp per engine
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust Approximately 18,800 hp total
2,800 kg 6,170 lb MTOW 76,610 kg 168,900 lb
1,010 nm 1,871 km range 4,600 km 2,485 nm
180 knots 105 mph cruise speed 660 km/h 410 mph
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.