Lavochkin La-5UTI
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type | Trainer |
Crew | 2 |
| Manufacturer(s) | Lavochkin |
||
| Production | 9920 (all models) |
||
| First Flight | March 1942 (La-5) |
Introduction | July 1942 (La-5) |
| Variants | |||
| LaG-5 | Developmental Designation | ||
| La-5 | Production Designation, fitted with an ASh-82A engine of 1650hp | ||
| La-5F | Fitted with an ASh-82F engine of 1650hp | ||
| La-5FN | "Definitive" La-5 Model; appearing in 1943; fitted with an ASh-82FN engine of 1850hp; provision for 4 x 3.23-in rockets OR 2 x PTAB anti-armor weapons along with the standard 2 x 20mm cannon battery; later production aircraft to feature upgunned 23mm cannons. | ||
| La-5UTI | Two-Seat Conversion Trainer | ||
| DIMENSIONS | |||
| Empty Weight | ? kg |
Loaded Weight | 3210 kg |
| Max takeoff weight | ? kg |
Length | 8.67 m |
| Wingspan | 9.8 m |
Wing area | 17.62 m² |
| Height | 2.54 m |
Wing Loading | 187 kg/m² |
| ARMAMENT | |||
| Main Guns | 1 × 20 mm ShVAK cannons (*) |
Ammunition Carried | 170, 200 |
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | - |
||
(*) Above engine
| POWERPLANT | |||
| Engine | 1 × Shvetsov ASh-82F |
Type & Displacement | 14-cylinder two-row radial, Air
, 41.21 L |
| Horsepower (maximum) | 1650
hp |
Power/Weight Ratio | 514 hp / ton * |
| Fuel Capacity | 462 L (Internal)
|
||
(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 600 km/h
at altitude |
Cruise Speed | ? km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 9550 m |
| Rate of Climb | 18 m/s at sea level |
Range | 765 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | Aviation of World War II | - |
|
Drawings |
