FORCETALLY
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At a glance
Measured figures
Bulldog Series 120 · Length
Single source23 ft 3.06 in (7.0881 m)[source]
Configuration
| Specification | Scottish Aviation Bulldog | Soko G-2 Galeb |
|---|---|---|
| Type | Basic trainer with aerobatic capability[source]Bulldog | Jet trainer and ground-attack[source]G-2 Galeb |
| Manufacturer | Beagle Aircraft / Scottish Aviation[source]Bulldog | SOKO[source]G-2 Galeb |
| Status | Active[source]Bulldog | Limited service[source]G-2 Galeb |
| Primary user | Royal Air Force |
G-2-A · Length
10.34 m (33 ft 11 in)[source]
Empty; Bulldog Series 120 · Empty weight
Single sourceMaximum take-off; Bulldog Series 120 · Max takeoff weight
Single source1,475 lb (669 kg)[source]
2,350 lb (1,066 kg)[source]
Empty; G-2-A · equipped
Single sourceMaximum take-off; G-2-A · clean aerobatic trainer
Single sourceBulldog Series 120 · 1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming IO-360-A1B6 4-cylinder air-cooled horizontally-opposed piston engine, 200 hp (150 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 | 328[source]Bulldog | 248[source]G-2 Galeb |
|---|
| Manufactured | 1969–1982[source]Bulldog | 1965–1985[source]G-2 Galeb |
|---|
| Introduction date | 1971[source]Bulldog | — |
|---|
| First flight | 19 May 1969[source]Bulldog | 3 July 1961[source]G-2 Galeb |
|---|
| Developed from | Beagle Pup[source]Bulldog | — |
|---|
| Aspect ratio | 8.4[source] | 5.55[source] |
|---|
| Airfoil | NACA 63 2 615[source] | root: NACA 64A213.5 ; tip: NACA 64A212[source] |
|---|
| Propellers | 2-bladed Hartzell constant speed propeller[source] | — |
|---|
| Stall speed | 54 kn (62 mph, 100 km/h)[source] | 158 km/h (98 mph, 85 kn) flaps down and airbrakes out[source] |
|---|
| Never exceed speed | 185 kn (213 mph, 343 km/h)[source] | — |
|---|
| g limits | + 6g - 3g, with no longer than 15 seconds sustained inverted flight.[source] | + 8 - 4[source] |
|---|
| Wing loading | 18.2 lb/sq ft (89 kg/m 2 )[source] | — |
|---|
| National origin | United Kingdom[source] | 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 |
|---|
| Fuel capacity | — | 780 kg (1,720 lb) internal + 340 kg (750 lb) in two optional wing-tip drop tanks[source] |
|---|
| Endurance | — | 2 hours30 minutes at 7,000 m (23,000 ft)[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] |
|---|