La-152 (Type 4) by S.A.LavochkinJet 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).
| 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 | 267kg/m2 | |||||||||||
| Trust 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 | |||||||||||
| Modified February 17, 1998
by Alexandre Savine |
Back to Main Gate |