FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Length
Single source6.942 m (22 ft 9 in)[source]
G-2-A · Length
Single sourceConfiguration
| Specification | Morane-Saulnier MS.230 | Soko G-2 Galeb |
|---|---|---|
| Type | Elementary Trainer[source] | Jet trainer and ground-attack[source]G-2 Galeb |
| Manufacturer | Morane-Saulnier[source] | SOKO[source]G-2 Galeb |
| Primary user | Armée de l'Air Flight School, Reims, France[source] | — |
| Number built | 1000+[source] | 248[source] |
10.34 m (33 ft 11 in)[source]
1 × Salmson 9AB 9-cylinder air-cooled radial piston engine
Single source1 × Salmson 9AB 9-cylinder air-cooled radial piston engine, 170 kW (230 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 · 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.
| First flight | February 1929[source] | 3 July 1961[source]G-2 Galeb |
|---|
| Fuel capacity | 220 L (58 US gal; 48 imp gal) jettison-able fuselage tank with a 22 L (5.8 US gal; 4.8 imp gal) centre-section gravity tank[source] | 780 kg (1,720 lb) internal + 340 kg (750 lb) in two optional wing-tip drop tanks[source] |
|---|
| Propellers | 2-bladed fixed-pitch wooden propeller[source] | — |
|---|
| Never exceed speed | 260 km/h (160 mph, 140 kn)[source] | — |
|---|
| Time to altitude | 3,000 m (9,800 ft) in 11 minutes 18 seconds[source] | 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] |
|---|
| Wing loading | 61.3 kg/m 2 (12.6 lb/sq ft)[source] | — |
|---|
| Power/mass | 0.1429 kW/kg (0.0869 hp/lb)[source] | — |
|---|
| National origin | — | Yugoslavia[source]G-2 Galeb |
|---|
| Designer | — | Aeronautical Technical Institute[source]G-2 Galeb |
|---|
| Status | — | Limited service[source]G-2 Galeb |
|---|
| Primary users | — | Yugoslav Air Force Libyan Air Force[source]G-2 Galeb |
|---|
| Manufactured | — | 1965–1985[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] |
|---|
| 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] |
|---|
| 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] |
|---|