Mitsubishi A6M Zero vs. lockheed C-130 hercules

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Mitsubishi A6M Zero versus lockheed C-130 hercules
9.06 m 29 ft 9 in length 29.79 m 97 ft 9 in
3.05 m 10 ft height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine Approximately 4,590 hp per engine
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust Approximately 18,360 hp total
2,800 kg 6,170 lb MTOW 70,307 kg 155,000 lb
1,010 nm 1,871 km range 3,760 km 2,031 nm
180 knots 105 mph cruise speed 540 km/h 335 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.