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 |
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capacity |
based on configuration |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.