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Soko G-4 Super Galeb
The Soko G-4 Super Galeb (English: ''Super Seagull'') is a single-engine, advanced jet trainer and light ground-attack aircraft and light fighter designed by the Aeronautical Technical Institute and manufactured by SOKO of Yugoslavia.〔https://fas.org/man/dod-101/sys/ac/row/galeb.htm〕
==Development==
The G-4 Super Galeb was developed as a replacement for the G-2 Galeb, which had been the most commonly used jet trainer aircraft of the Yugoslav Air Force up until 1985. The first of two prototypes was completed by early 1978. Following completion of the initial testing phase, the first flight was achieved on 17 July 1978 and the first of six pre-production aircraft on 17 December 1980. These and the first prototype were designated G-4 PPP, and had fixed tailplanes with inset elevators and no anhedral.〔(SOKO Super Galeb G-4 (Super Seagull) Light Atack/Advanced Trainer )〕 Production examples (and the second prototype) were designated G-4 and featured an all-moving anhedral tailplane and comprehensive avionics improvements. The G-4 first flew in 1983 and has been ordered in large numbers for the Yugoslav Air Force. The G-4 features a low wing monoplane design with slightly tapered wings.
The aircraft is 12.25m long and 4.3m high, with a wingspan of 9.88m.〔 It weighs 3,250 kg when empty and can carry 1,882 kg of fuel. The aircraft is fitted with a short nose cone, rounded fuselage, conventional empennage, semicircular air intakes, vertical tailfins, rudder, ailerons, horizontal stabilisers and fuel tanks at the square tips. The G-4 its performance is considerably improved by the introduction of a more powerful version of the Rolls-Royce Viper 632-46 turbojet.〔 The cockpit is fitted with two ejection seats with the rear seat slightly elevated to render all round clear visibility.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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