| Manufacturer |
SOKO |
| Description |
The Soko G-4 Super Galeb (from ), also referred to as N-62, is a Yugoslav single-engine, advanced jet trainer and light ground-attack aircraft designed by the Aeronautical Technical Institute at Žarkovo and manufactured by the SOKO aircraft factory in Mostar. |
| ICAO Code |
G4SG |
| First Flight |
1978-07-17 |
| Entry Into service |
1983-01-01 |
| Production End |
1991-01-01 |
| Designer |
Aeronautical Technical Institute |
| Type |
Military trainer aircraft |
| Length (m) |
12.25 |
| Height (m) |
4.3 |
| Cockpit Crew |
2 |
| Max Speed (km/h) |
910 |
| Cruise Speed (km/h) |
550 |
| Min Speed (km/h) |
180 |
| Max Ceiling (m) |
12850 |
| Rate of Climb (m/s) |
31 |
| Armament |
1 × GSh-23L 23 mm cannon in ventral gun pod.; 2 × inner pylons 350 kg (770 lb) capacity.; 2 × outer pylons 250 kg (550 lb) capacity.; 1 × centerline pylon 400 kg (880 lb) capacity (G-4M).; 2 × wingtip missile rails (G-4M). |
| National Origin |
Yugoslavia |
| Number Built |
85 |
| Powerplant Description |
1 × Rolls-Royce Viper 632-46 turbojet, 17.8 kN thrust each |
| Primary Users |
Serbian Air Force, Myanmar Air Force , Montenegrin Air Force (historical) , Yugoslav Air Force (historical) |
| Status |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Soko_G-4_Super_Galeb |
| Flat Wing Span (m) |
9.88 |
| Flat Wing Area (m²) |
19.5 |
| Flat Wing Aspect Ratio |
5.01 |
| Wake Category |
L |
| Aircraft Engine |
Armstrong Siddeley Viper |
| Number of Engines |
1 |