FORCETALLY
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At a glance
Measured figures
X-26A Frigate · Length
Single source26 ft 9 in (7.92 m)[source]
Bulldog Series 120 · Length
Configuration
| Specification | Schweizer X-26 Frigate | Scottish Aviation Bulldog |
|---|---|---|
| Crew | two[source] | 2, model 101 has 3[source] |
| Type | Research and training aircraft[source] | Basic trainer with aerobatic capability[source]Bulldog |
| National origin | United States[source] | United Kingdom[source] |
| Manufacturer | Schweizer[source] |
23 ft 3.06 in (7.0881 m)[source]
Bulldog Series 120 · Range
Single source540 nmi (620 mi, 1,000 km)[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]
Bulldog Series 120 · Service ceiling
Single source16,000 ft (4,900 m)[source]
Bulldog Series 120 · 1,034 ft/min (
Single source1,034 ft/min (5.25 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Beagle Aircraft / Scottish Aviation[source]Bulldog |
| Designer | Ernie and William Schweizer[source] | — |
|---|
| Primary user | United States Navy[source] | Royal Air Force[source]Bulldog |
|---|
| Number built | 7?[source] | 328[source]Bulldog |
|---|
| First flight | July 1967[source] | 19 May 1969[source]Bulldog |
|---|
| Developed from | Schweizer SGS 2-32[source] | Beagle Pup[source]Bulldog |
|---|
| Status | 1: Unknown. #2 Operational as a glider at Mile High Gliding[source] | Active[source]Bulldog |
|---|
| Introduction date | 1967[source] | 1971[source]Bulldog |
|---|
| Retired | 1969 as X-26B[source] | — |
|---|
| Wing aspect ratio | 18[source] | — |
|---|
| Wing loading | 7.9 lb/sq ft (39 kg/m 2 )[source] | 18.2 lb/sq ft (89 kg/m 2 )[source] |
|---|
| Power/mass | 0.07 hp/lb (0.12 kW/kg)[source] | — |
|---|
| Rate of sink | 0.6 m/s (120 ft/min)[source] | — |
|---|
| Manufactured | — | 1969–1982[source]Bulldog |
|---|
| Aspect ratio | — | 8.4[source] |
|---|
| Airfoil | — | NACA 63 2 615[source] |
|---|
| Propellers | — | 2-bladed Hartzell constant speed propeller[source] |
|---|
| Stall speed | — | 54 kn (62 mph, 100 km/h)[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] |
|---|