FORCETALLY
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At a glance
Measured figures
1 × Allison 250 -B17-D turboprop
Single source1 × Allison 250 -B17-D turboprop , 313 kW (420 hp)[source]
G-2-A · 1 × DMB license-built Rolls-Royce Viper ASV.11 Mk 22-6 turbojet engine thrust
Single source1 × DMB license-built Rolls-Royce Viper ASV.11 Mk 22-6 turbojet engine, 11.12 kN (2,500 lbf) thrust[source]
G-2-A · Wing area
Single source19.43 m 2 (209.1 sq ft)[source]
G-2-A · 4,494 ft/min
Single source22.83 m/s (4,494 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Soko G-2 Galeb | Thai Aviation Industries RTAF-6 |
|---|---|---|
| Type | Jet trainer and ground-attack[source]G-2 Galeb | Trainer aircraft[source] |
| National origin | Yugoslavia[source]G-2 Galeb | Thailand[source] |
| Manufacturer | SOKO[source]G-2 Galeb | Thai Aviation Industry[source] |
| Designer | Aeronautical Technical Institute[source]G-2 Galeb | — |
| Status | Limited service[source]G-2 Galeb | In service, in production[source] |
| Primary users | Yugoslav Air Force Libyan Air Force[source]G-2 Galeb | — |
| Number built | 248[source]G-2 Galeb | 3 (2017), 25 reported built[source] |
| Manufactured | 1965–1985[source]G-2 Galeb | 2014–present[source] |
| First flight | 3 July 1961[source]G-2 Galeb | 14 June 2012[source] |
| Variant | J-21 Jastreb[source]G-2 Galeb | — |
| Aspect ratio | 5.55[source] | — |
| Airfoil | root: NACA 64A213.5 ; tip: NACA 64A212[source] | — |
| Fuel capacity | 780 kg (1,720 lb) internal + 340 kg (750 lb) in two optional wing-tip drop tanks[source] | — |
| Stall speed | 158 km/h (98 mph, 85 kn) flaps down and airbrakes out[source] | — |
| Endurance | 2 hours30 minutes at 7,000 m (23,000 ft)[source] | — |
| g limits | + 8 - 4[source] | — |
| Time to altitude | 3,000 m (9,800 ft) in 2 minutes 24 seconds 6,000 m (20,000 ft) in 5 minutes 30 seconds 9,000 m (30,000 ft) in 10 minutes 12 seconds[source] | — |
| Take-off run | 490 m (1,610 ft) on grass[source] | — |
| Landing run | 400 m (1,300 ft) on grass[source] | — |
| Take-off run to 15 m (49 ft) | 640 m (2,100 ft)[source] | — |
| Landing run from 15 m (49 ft) | 710 m (2,330 ft)[source] | — |
| Guns | 2× 12.7 mm (0.500 in) machine guns in nose with 80 rpg[source] | — |
| Hardpoints | 4 with a capacity of 300 kg (661 lb) total[source] | 4 with a capacity of up to 68 kg (150 lb) on inner, 100 lb (45 kg) on outer[source] |
| Primary user | — | Royal Thai Air Force[source] |
| Introduction date | — | 2014[source] |
| Developed from | — | SIAI-Marchetti SF.260[source] |