| Manufacturer |
Blackburn Aircraft |
Armstrong Whitworth |
| Description |
The Blackburn Type E was a development of the earlier Blackburn Mercury single-engined monoplanes, but was innovative in its use of steel tubing to construct the fuselage. |
The Armstrong Whitworth Wolf was a British two-seat reconnaissance aircraft ordered by the Royal Air Force in 1923. |
| First Flight |
1912-04-01 |
1923-01-19 |
| Entry Into service |
|
1923-01-01 |
| Production End |
|
1929-01-01 |
| Service End |
|
1931-01-01 |
| Designer |
Robert Blackburn |
Armstrong Whitworth |
| Type |
|
Trainer |
| Length (m) |
9.4488 |
9.4488 |
| Height (m) |
|
3.9624 |
| Cockpit Crew |
|
2 |
| Max Speed (km/h) |
128.7475 |
177.0278 |
| Max Ceiling (m) |
|
4617.72 |
| Armament |
|
1 × fixed, forward-firing .303 in (7.7 mm) Vickers machine gun; 1 × .303 in (7.7 mm) Lewis Gun in Scarff ring for observer |
| Endurance (h) |
5 |
3 |
| National Origin |
United Kingdom |
|
| Number Built |
2 |
6 |
| Powerplant Description |
1 × Renault 70 hp air-cooled V-8 |
1 × Armstrong Siddeley Jaguar III 14-cylinder two-row air-cooled radial engine, 261 kW (350 hp) each |
| Primary Users |
|
Royal Air Force, Royal Aircraft Establishment |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Blackburn_Type_E |
en.wikipedia.org/wiki/Armstrong_Whitworth_Wolf |
| Flat Wing Span (m) |
11.5824 |
11.8872 |
| Flat Wing Area (m²) |
26.9419 |
45.3367 |
| Aircraft Engine |
Renault 70 hp |
Armstrong Siddeley Jaguar |
| Number of Engines |
1 |
1 |