Airbus A310-300 vs. Soko G-2 Galeb

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Airbus A310-300 versus Soko G-2 Galeb
46.66 m 153 ft 1 in length 10.34 m 33 ft 11 in
15.8 m 51 ft 10 in height 3.28 m 10 ft 9 in
43.9 m 144 ft wingspan 11.62 m 38 ft 1 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
52,000 lb thrust per engine 2,500 lb
104,000 lb total thrust 2,500 lb
148,768 kg 328,000 lb MTOW 4,300 kg 9,480 lb
8,050 km 4,348 nm range 1,242 km 671 nm
482 knots 279 mph cruise speed 730 km/h 454 mph
190-230 passengers capacity Fuel capacity: 1,120 ltr
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.