| Technical data | |
|---|---|
| Type | La-150m |
| Function | Pre-production fighter |
| Year | 1946 |
| Crew | 1 |
| Engines | 1*900kg RD-10 |
| Length | 9.42m |
| Wingspan | 8.20m |
| Wing area | 12.15m2 |
| Empty weight | 2369kg |
| Loaded weight | 3338kg |
| Wing Load (kg/m2) | 275 |
| Thrust Weight |
0.270 |
| Speed at 0m | 760km/h |
| Speed at 5000m | 805km/h |
| Range | 500km |
| Flight Endurance | 48min |
| Ceiling | 12500m |
| Climb | |
| 5000m | 7.2min |
| Armament | |
| Guns | 2*cannons 23mm NS-23 |
La-150M by S.A.Lavochkin
Pre-production series development of the La-150. Fuel tanks capacity was increased, tailfin enlarged. Curved windscreen was replaced by the flat one (more technological). As a result of all those changes, flight weight increased by 300-400kg. Aircraft still was unable to fulfill all requirements (TTKh).
At the same time handling problems were fixed. Small pre-production butch of the La-150M was sent to fighter regiments for evaluation. Regiment tests continued until September 1947. La-150M was not accepted by military and remained an experimental aircraft.
| Predecessors | Modifications |
|---|---|
 La-150 Type 3 |
 La-150F |
| References | Links |
|---|---|
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