| Technical data | |
|---|---|
| Type | La-152 |
| Function | Experimental fighter |
| Year | 1946 |
| Crew | 1 |
| Engines | 1*900kg RD-10 |
| Length | 9.12m |
| Wingspan | 8.20m |
| Wing area | 12.15m2 |
| Empty weight | 2310kg |
| Loaded weight | 3239kg |
| Wing Load (kg/m2) | 267 |
|
Thrust
Weight |
0.278 |
| Speed at 0m | 730km/h |
| Speed at 5000m | 778km/h |
| Flight Endurance | 54min |
| Range | 500km |
| Ceiling | 12500m |
| Climb | |
| 5000m | 6.5min |
| Armament | |
| Guns | 3*cannons 23mm NS-23 |
La-152 (Type 4) by S.A.Lavochkin
Jet fighter with straight wing, built almost in parallel with the La-150. Experience in the La-150 development was used, because La-152 had slightly later schedule. It had similar size, thinner laminar flow wing and more powerful armament. Airframe was lighter, fuel capacity slightly larger (563kg against 553kg on the La-150).
Flight tested during October 1946 - August 1947, not accepted for production.
| Predecessors | Modifications | |
|---|---|---|
 La-150 Type 3 |
La-154 |
 La-156 Type 5 |
| References | Links |
|---|---|
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