Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Bulldog Series 120 · Length
Single sourceConfiguration
| Specification | Grob G 115 | Scottish Aviation Bulldog |
|---|---|---|
| Type | Basic trainer[source] | Basic trainer with aerobatic capability[source]Bulldog |
| Manufacturer | Grob Aircraft[source] | Beagle Aircraft / Scottish Aviation[source]Bulldog |
| Status | active[source] | Active[source]Bulldog |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
23 ft 3.06 in (7.0881 m)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single source250 km/h (160 mph, 130 kn)[source]
178 km/h (111 mph, 96 kn) (long range cruising speed)[source]
Maximum; Bulldog Series 120 · Maximum speed
Single source130 kn (150 mph, 240 km/h)[source]
G 115E · 1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)[source]
Bulldog 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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Manufactured | 1985–present[source] | 1969–1982[source]Bulldog |
|---|
| Introduction date | 1999[source] | 1971[source]Bulldog |
|---|
| First flight | November 1985[source] | 19 May 1969[source]Bulldog |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
|---|
| Aspect ratio | 8.2:1[source] | 8.4[source] |
|---|
| Airfoil | Eppler 696[source] | NACA 63 2 615[source] |
|---|
| Propellers | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] | 2-bladed Hartzell constant speed propeller[source] |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | 54 kn (62 mph, 100 km/h)[source] |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | 185 kn (213 mph, 343 km/h)[source] |
|---|
| g limits | + 6.0/ - 3.0[source] | + 6g - 3g, with no longer than 15 seconds sustained inverted flight.[source] |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| Primary user | — | Royal Air Force[source]Bulldog |
|---|
| Number built | — | 328[source]Bulldog |
|---|
| Developed from | — | Beagle Pup[source]Bulldog |
|---|
| Wing loading | — | 18.2 lb/sq ft (89 kg/m 2 )[source] |
|---|
| National origin | — | United Kingdom[source] |
|---|