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Measured figures
G-2-A · Length
Single source10.34 m (33 ft 11 in)[source]
Configuration
| Specification | L-15Z | Soko G-2 Galeb |
|---|---|---|
| Variant description | L-15Z : Designation of L-15 advanced fighter trainer in Zambian Air Force service.[source]Only the source-declared variant L-15Z | — |
| Type | — | Jet trainer and ground-attack[source]G-2 Galeb |
| National origin | — | Yugoslavia[source]G-2 Galeb |
| Manufacturer | — | SOKO[source]G-2 Galeb |
| Designer | — | Aeronautical Technical Institute[source] |
G-2-A · with tip-tanks
Single source11.62 m (38 ft 1 in) with tip-tanks[source]
G-2-A · Height
Single source3.28 m (10 ft 9 in)[source]
Maximum; G-2-A · at sea level
Single source756 km/h (470 mph, 408 kn) at sea level[source]
G-2-A · at 9,000 m (30,000 ft) with full tip-tanks
Single source669 km (416 mi, 361 nmi) at 9,000 m (30,000 ft) with full tip-tanks[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 · Service ceiling
Single source12,000 m (39,000 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.
| Status | — | Limited service[source]G-2 Galeb |
|---|
| Primary users | — | Yugoslav Air Force Libyan Air Force[source]G-2 Galeb |
|---|
| Number built | — | 248[source]G-2 Galeb |
|---|
| Manufactured | — | 1965–1985[source]G-2 Galeb |
|---|
| First flight | — | 3 July 1961[source]G-2 Galeb |
|---|
| 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] |
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| Guns | — | 2× 12.7 mm (0.500 in) machine guns in nose with 80 rpg[source] |
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| Hardpoints | — | 4 with a capacity of 300 kg (661 lb) total[source] |
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