Lockheed P-2 Neptune vs. Soko G-2 Galeb

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Lockheed P-2 Neptune versus Soko G-2 Galeb
30.17 m 99 ft 0 in length 10.34 m 33 ft 11 in
10.15 m 33 ft 4 in height 3.28 m 10 ft 9 in
33.53 m 110 ft wingspan 11.62 m 38 ft 1 in
2 x Wright R-3350 radial engines engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
Approximately 3,700 hp thrust per engine 2,500 lb
Approximately 7,400 hp total thrust 2,500 lb
27,216 kg 60,000 lb MTOW 4,300 kg 9,480 lb
7,885 km 4,259 nm range 1,242 km 671 nm
300 mph 483 km/h cruise speed 730 km/h 454 mph
based on configuration 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.