Airbus A310-300 vs. Polikarpov I-16

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Airbus A310-300 versus Polikarpov I-16
46.66 m 153 ft 1 in length 6.13 m 20 ft 1 in
15.8 m 51 ft 10 in height 3.25 m 10 ft 8 in
43.9 m 144 ft wingspan 9 m 29 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1x Shvetsov M-25 radial engine
52,000 lb thrust per engine 1000 hp
104,000 lb total thrust 1000 hp
148,768 kg 328,000 lb MTOW 2,060 kg 4,540 lb
8,050 km 4,348 nm range 248 mi 216 nm
482 knots 279 mph cruise speed 180 mph 290 km/h
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.