Flat Wing Aspect Ratio
5.01
Entry Into service
1983-01-01
Maximum Take-Off Weight
6.33 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Soko G-4 Super Galeb |
6.33 |
1900 |
Similar airplanes
All data (30 fields)
- Name
- Soko G-4 Super Galeb
- 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