Polikarpov I-16 vs. Airbus H225 Super Puma

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Polikarpov I-16 versus Airbus H225 Super Puma
6.13 m 20 ft 1 in length 14.06 m 46 ft 2 in
3.25 m 10 ft 8 in height 4.38 m 14 ft 4 in
9 m 29 ft 6 in wingspan
1x Shvetsov M-25 radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
1000 hp thrust per engine 2,778 hp
1000 hp total thrust 5,556 hp
2,060 kg 4,540 lb MTOW 11,000 kg 24,251 lb
248 mi 216 nm range 857 km 463 nm
180 mph 290 km/h 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.