Curtiss-Wright SNC-1
| GENERAL DATA | |||
| Other Designation(s) | Falcon,
CW-22N |
||
| Type | Scout
and Advanced Trainer |
Crew | 2 |
| Manufacturer(s) | Curtiss-Wright
Corporation |
||
| Production | 442: 305 SNC-1(CW-22N),
100 CW-22B, 36 CW-22, 1 CW-A22 (Prototype) |
||
| First Flight | 1940 |
Introduction | 1942 |
| DIMENSIONS | |||
| Length | 8.23 m |
Empty Weight | 1241 kg |
| Wingspan | 10.67 m |
Loaded Weight | 1718 kg |
| Height | 3.02 m |
Max takeoff weight | ? kg |
| Wing area | 16.14 m² |
Wing Loading | 106.456 kg/m² |
| ARMAMENT | |||
| Main Guns | 2 × .30 in (7.62 mm) M1919
Browning * |
Ammunition Carried | 2 x 200 |
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | - |
||
(*) one, synchronized to fire through the propeller & other, flexibly mounted
| POWERPLANT | |||
| Engine | 1 x Wright R-975-28 Whirlwind |
Type & Displacement | 9-cylinder air-cooled radial, 15.93
L |
| Horsepower (maximum) | 420 hp to 450 hp* |
Power/Weight Ratio | 244.47-261.93 hp / ton ** |
| Fuel Capacity | 362 L
|
||
(*) for take-off, (**) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 319 km/h at sea level |
Cruise Speed | 309 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 6600 m |
| Rate of Climb | 8.4 m/s |
Range | 835 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | airwar.ru | - |
|
Drawings |
