/2-Airplanes/Allies/UK/1-Fighters/Data/AW-FK10.htm | Update: -
Armstrong Whitworth F.K.10
| GENERAL DATA | |||
| Type |
Fighter
|
||
| Manufacturer(s) | Armstrong Whitworth |
||
| Prototype first flight | Late 1916, early 1917 |
Introduction | 1917 |
| Production | 9 (1 F.K.9 + 8 F.K.10) |
Crew | 2 |
| DIMENSIONS | |||
| Length | 6.78 m |
Empty Weight | 561 kg |
| Wingspan | 8.48 m |
Loaded Weight | 916 kg |
| Height | 3.51 m |
Max takeoff weight | ? kg |
| Wing area | 36.27 m² |
Wing loading | ? kg/m² |
| ARMAMENT | ||||
| Guns | 1× .303 in (7.7 mm) Vickers
gun* |
Ammunition Carried |
? |
|
1× .303 in (7.7 mm) Lewis gun** |
? |
|||
| Other Armament | - |
|||
(*) forward-firing, synchronised, (**) in observer's cockpit
| POWERPLANT | |||
| Engine | 1 ×
Clerget 9B |
Type & Displacement | 9-cylinder rotary engine, 16.29
L |
| Horsepower | 130 hp |
Power/Weight Ratio | 141.92 hp / ton ** |
| Fuel Capacity | 200 L
|
||
(*) with the maximum loaded weight
| PERFORMANCES | |||
| Maximum Speed | 135 km/h
at 2000 m 169 km/h at ground level |
Rate of Climb | 2.32 m/s |
| Range | 340 km |
Service Ceiling | 3000 m |
| Sources | |||
| Wikipédia | militaryfactory.com | ||
Drawings |
