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At a glance
Measured figures
DH.87B · Length
Single source24 ft 11 + 1 ⁄ 2 in (7.61 m)[source]
G-2-A · Length
Single sourceConfiguration
| Specification | De Havilland Hornet Moth | Soko G-2 Galeb |
|---|---|---|
| Type | Trainer and Tourer[source] | Jet trainer and ground-attack[source]G-2 Galeb |
| Manufacturer | de Havilland[source] | SOKO[source]G-2 Galeb |
| Status | In limited service[source] | Limited service[source]G-2 Galeb |
| Primary user | private owner pilots[source] |
10.34 m (33 ft 11 in)[source]
DH.87B · Width
Single source10 ft 9 + 1 ⁄ 2 in (3.29 m)[source]
Cruise; DH.87B · at 1,000 ft (305 m)
Single sourceMaximum; DH.87B · at sea level
Single source124 mph (200 km/h, 108 kn) at sea level[source]
105 mph (169 km/h, 91 kn) at 1,000 ft (305 m)[source]
Maximum; G-2-A · at sea level
Single source756 km/h (470 mph, 408 kn) at sea level[source]
DH.87B · 1 × de Havilland Gipsy Major I 4-cylinder air-cooled inverted in-line piston engine
Single source1 × de Havilland Gipsy Major I 4-cylinder air-cooled inverted in-line piston engine, 130 hp (97 kW)[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 164[source] | 248[source]G-2 Galeb |
|---|
| Manufactured | 1935–1938[source] | 1965–1985[source]G-2 Galeb |
|---|
| First flight | 9 May 1934[source] | 3 July 1961[source]G-2 Galeb |
|---|
| Capacity | 1 passenger / trainee[source] | — |
|---|
| Airfoil | RAF 15[source] | root: NACA 64A213.5 ; tip: NACA 64A212[source] |
|---|
| Fuel capacity | 35 imp gal (42 US gal; 159 L) fuel in fuselage 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 propeller[source] | — |
|---|
| Stall speed | 40 mph (64 km/h, 35 kn)[source] | 158 km/h (98 mph, 85 kn) flaps down and airbrakes out[source] |
|---|
| Time to altitude | 5,000 ft (1,524 m) in 8 minutes 45 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 | 7.97 lb/sq ft (38.9 kg/m 2 )[source] | — |
|---|
| Power/mass | 0.067 hp/lb (0.110 kW/kg)[source] | — |
|---|
| National origin | — | Yugoslavia[source]G-2 Galeb |
|---|
| Designer | — | Aeronautical Technical Institute[source]G-2 Galeb |
|---|
| Primary users | — | Yugoslav Air Force Libyan Air Force[source]G-2 Galeb |
|---|
| Variant | — | J-21 Jastreb[source]G-2 Galeb |
|---|
| Aspect ratio | — | 5.55[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] |
|---|