Chengdu J-20 vs. Airbus H225 Super Puma

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Chengdu J-20 versus Airbus H225 Super Puma
20.4 m 66 ft 11 in length 14.06 m 46 ft 2 in
4.45 m 14 ft 7 in height 4.38 m 14 ft 4 in
13.01 m 42 ft 8 in wingspan
2x Saturn 117S or Xian WS-15 engines 2 x Turbomeca Makila 2A turboshaft engines
30,000-32,000 lbs thrust per engine 2,778 hp
60,000-64,000 lbs total thrust 5,556 hp
37,000 kg 81,600 lb MTOW 11,000 kg 24,251 lb
3,200 nm 5,926 km range 857 km 463 nm
1,305 mph 2,100 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.