SOKO G-2 Galeb
Summary
Category | Training aircraft |
Origin country | 🇳🇱 Ex-Yugoslavia |
First flight | 31 July 1961 |
Year of introduction | 1965 |
Number produced | 248 units |
Average unit price | $0.2 million |
Description
In 1957, the Aeronautical Technical Institute (VTI) of Yugoslavia initiated the Galeb's design, aiming to replace the Lockheed T-33 Shooting Star jet trainer then in service. The aircraft was intended for ab initio, intermediate, and advanced training missions. SOKO, an aircraft manufacturer in Mostar, Bosnia and Herzegovina, established in 1951, handled primary manufacturing. The Galeb's development was a collaborative effort between Yugoslavia and the United Kingdom; a significant number of components, including the Armstrong Siddeley Viper turbojet engine, ejector seats, and navigational fittings, were sourced from British aerospace manufacturers. Rolls-Royce Limited sponsored the engine development. Two prototypes were constructed; the first, Galeb 1, made its maiden flight on 3 July 1961, piloted by Ljubomir Zekavica. Following a full-size wooden mock-up, the second prototype, Galeb 2, was constructed. In 1964, mass production commenced, making it the first indigenously developed jet aircraft in Yugoslavia. A total of 248 Galeb aircraft were produced, with 132 used by the Yugoslav Air Force. Production of updated aircraft for export to Libya was extended until mid-1983.
The G-2 Galeb is a versatile trainer aircraft designed to fulfill a wide array of training missions. Operated by a crew of two, a candidate pilot and an instructor, the aircraft features a tandem cockpit layout and Folland Type 1-B lightweight ejector seats for both crew members. Power is provided by a single Armstrong Siddeley Viper II Mark 22/6 turbojet engine, delivering up to 2,500lb of thrust, facilitating rapid and stall-free acceleration. Constructed with a conventional stressed-skin design using frames and bulkheads, the Galeb incorporates an all-metal straight wing complete with tip tanks. The aircraft is equipped with a hydraulic system featuring an engine-driven hydraulic pump and a 24-volt battery powers its electrical systems. The G-2 Galeb is equipped with two 12.7 mm machine guns in the nose, each with 80 rounds. Furthermore, the aircraft features four underwing hardpoints with a total capacity of 300 kg for external stores, enabling the Galeb to carry a variety of munitions, including bombs and rockets, for light attack or weapons training missions.
The G-2-A Galeb served as the standard trainer with the Yugoslav Air Force, extensively used for school-combat training of Military Air Force Academy cadets. Its ease of handling and maintenance made it popular among both students and technicians, with aircraft regularly achieving 5,000 flight hours. An export variant, the G-2-AE, was introduced in late 1974 for Libya and Zambia. During the Bosnian War, Galeb aircraft saw combat use with the 105th Fighter-Bomber Regiment over Bosnia-Herzegovina, while reports indicate the deployment of a few aircraft to Zaire during the First Congo War, flown by Serbian mercenaries. The Libyan Air Force also operated the Galeb, employing it in ground attack missions during the 2011 Libyan civil war; some were destroyed by NATO forces enforcing a no-fly zone. The aircraft continued in service with the Libyan Dawn forces during the Second Libyan Civil War, though the operational status remains uncertain.
Main Variants:
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G-2-A: The standard two-seat advanced jet trainer and light attack aircraft operated by the Yugoslav Air Force.
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G-2A-E: A two-seat export version of the G-2-A, specifically designed for use by Libya and Zambia.
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G-2Š: An unarmed trainer variant of the G-2 Galeb, likely used for basic flight instruction.
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G3 Galeb-3: A prototype export version featuring a BMB (Rolls-Royce/Bristol Siddeley) Viper Mk 532 Turbojet engine, a modern cockpit, cameras in tip-tanks, doubled weapon load, JATO, and other modifications.
Technical specifications
Version: G-2A | |
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Maximum speed | 812 km/h (505 mph) |
Wing area | 19.4 m² (209.1 sqft) |
Wingspan | 11.6 m (38.1 ft) |
Height | 3.3 m (10.8 ft) |
Length | 10.3 m (33.9 ft) |
Service ceiling | 12000 m (39370 ft) |
Empty weight | 2620 kg (5776 lbs) |
Max. takeoff weight | 4300 kg (9480 lbs) |
Climb rate | 22.8 m/s (74.8 ft/s) |
Powerplant | 1 × turbojet Armstrong Siddeley Viper ASV.11 Mk 22-6 delivering 1134 kgp |
Current operating countries
Country | Units | ||
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Libya | 14 | |
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Serbia | 1 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
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