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Soko G-4 Super Galeb
(Super Seagull)
Role: - basic/advanced training
- ground supportFirst flown: 17 July 1978 First production: 1983, SOKO's Mostar plant Used by: 130 Yugoslavia (before the war)
12 Myanmar (Burma)
Technical data
G-4 Wing span: 9.88 meters (32 ft 5 in) Length: 11.862 meters (38 ft 11 in) Height: 4.28 meters (14 ft 0.5 in) Wing area: 19.5 sq meters Crew: 1 or 2 Weight empty: 3,134 kg Training weight: 4600 kg Take-off weight: 6.300 kg - max. weapon load (13,900 lb) Weapon load: 1700 kg underwing
1950 including detachable cannon podInternal fuel load: 1307 kg Maximum speed: 910 km/h (565 mph) Combat radius: 812 km with 625 liters of fuel in auxiliary fuel tanks Ceiling: 15,000 meters Rate of climb: 1,800 meters per minute Radar: None Engines: one license-built Rolls-Royce Viper 632-46 non-afterburning turbojet, rated at 1,814 (4000 lb or 17.8 kN) kg thrust
Weapons
one GSh-23L 23mm twin-barrel cannon in detachable pod under fuselage
Variants
G-4 Super Galeb
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