Chengdu J-20 vs. Grumman OV-1 Mohawk

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Chengdu J-20 versus Grumman OV-1 Mohawk
20.4 m 66 ft 11 in length 12.52 m 41 ft 1 in
4.45 m 14 ft 7 in height 3.89 m 12 ft 9 in
13.01 m 42 ft 8 in wingspan 14.63 m 48 ft
2x Saturn 117S or Xian WS-15 engines 2 x Lycoming T53 turboprop engines
30,000-32,000 lbs thrust per engine Approximately 1,100 hp each
60,000-64,000 lbs total thrust Approximately 2,200 hp total
37,000 kg 81,600 lb MTOW 14,950 lb 6,781 kg
3,200 nm 5,926 km range 1,690 km 913 nm
1,305 mph 2,100 km/h cruise speed 230 mph 370 km/h
capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.