Chengdu J-20 vs. de Havilland Canada DHC-2 Beaver

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Chengdu J-20 versus de Havilland Canada DHC-2 Beaver
20.4 m 66 ft 11 in length 13.56 m 44 ft 6 in
4.45 m 14 ft 7 in height 5 m 16 ft 5 in
13.01 m 42 ft 8 in wingspan 16.56 m 54 ft 4 in
2x Saturn 117S or Xian WS-15 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
30,000-32,000 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
60,000-64,000 lbs total thrust Approximately 6,200 hp (4,624 kW) total
37,000 kg 81,600 lb MTOW 24,200 lb 10,977 kg
3,200 nm 5,926 km range 2,535 km 1,369 nm
1,305 mph 2,100 km/h cruise speed 228 mph 367 km/h
capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.