| Technical data | |
|---|---|
| Type | La-15UTI |
| Function | Trainer |
| Year | 1949 |
| Crew | 2 |
| Engines | 1*1590kg RD-500 |
| Length | 9.56m |
| Wingspan | 8.83m |
| Wing area | 16.16m2 |
| Empty weight | 2805kg |
| Loaded weight | 3730kg |
| Wing Load (kg/m2) | 231 |
| Thrust to Weight |
0.43 |
| Speed at 0m | 960km/h |
| Speed at 5000m | 980km/h |
| Range | 910km |
| Flight Endurance | 1h30min |
| Ceiling | 12750m |
| Climb | |
| 5000m | 3.0min |
| Armament | |
| Guns | 1*12.7mm BS |
La-15UTI by S.A.Lavochkin
|
Two seat dual controls trainer modification of the La-15, armed with single 12.7mm BS machinegun. Flight performance was slightly worser than of the series single-seater.
Two were built, trials were completed in September 1949. Since the La-15 did not enter full-scale manufacturing, trainer production was cancelled.
| Predecessors | Modifications |
|---|---|
 La-15 |
None |
| References | Links |
|---|---|
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