Mitsubishi A6M Zero vs. Airbus H225 Super Puma

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Mitsubishi A6M Zero versus Airbus H225 Super Puma
9.06 m 29 ft 9 in length 14.06 m 46 ft 2 in
3.05 m 10 ft height 4.38 m 14 ft 4 in
12 m 39 ft 4 in wingspan
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine engines 2 x Turbomeca Makila 2A turboshaft engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine 2,778 hp
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust 5,556 hp
2,800 kg 6,170 lb MTOW 11,000 kg 24,251 lb
1,010 nm 1,871 km range 857 km 463 nm
180 knots 105 mph cruise speed 242 km/h 150 mph
capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.