| Manufacturer |
SOKO |
Boeing |
| 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. |
The McDonnell Douglas (now Boeing) T-45 Goshawk is a highly modified version of the British BAE Systems Hawk land-based training jet aircraft. |
| ICAO Code |
G4SG |
HAWK |
| First Flight |
1978-07-17 |
1988-04-16 |
| Entry Into service |
1983-01-01 |
1991-01-01 |
| Production End |
1991-01-01 |
2009-01-01 |
| Designer |
Aeronautical Technical Institute |
Boeing |
| Type |
Military trainer aircraft |
Naval trainer aircraft |
| Length (m) |
12.25 |
11.8872 |
| Height (m) |
4.3 |
3.9624 |
| Cockpit Crew |
2 |
2 |
| Max Speed (km/h) |
910 |
1005.635 |
| Cruise Speed (km/h) |
550 |
|
| Min Speed (km/h) |
180 |
|
| Max Ceiling (m) |
12850 |
12954 |
| Rate of Climb (m/s) |
31 |
40.64 |
| 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). |
Usually none: One hardpoint under each wing can be used to carry practice bomb racks (can carry up to 12 Mk-76 practice bombs), rocket pods, or fuel tanks. A centerline hardpoint can carry a cargo pod for crew baggage. |
| National Origin |
Yugoslavia |
United Kingdom |
| Number Built |
85 |
221 |
| Powerplant Description |
1 × Rolls-Royce Viper 632-46 turbojet, 17.8 kN thrust each |
1 × Rolls-Royce Turbomeca F405-RR-401 turbofan engine |
| Primary Users |
Serbian Air Force, Myanmar Air Force , Montenegrin Air Force (historical) , Yugoslav Air Force (historical) |
United States Navy |
| Status |
In service |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Soko_G-4_Super_Galeb |
en.wikipedia.org/wiki/McDonnell_Douglas_T-45_Goshawk |
| Flat Wing Span (m) |
9.88 |
9.144 |
| Flat Wing Area (m²) |
19.5 |
17.6609 |
| Flat Wing Aspect Ratio |
5.01 |
|
| Wake Category |
L |
M |
| Aircraft Engine |
Armstrong Siddeley Viper |
|
| Number of Engines |
1 |
1 |