| Modified February 17, 1998 |
|
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| Technical data | |
|---|---|
| Type | La-154 |
| Function | Experimental fighter |
| Year | 1946 |
| Crew | 1 |
| Engines | 1*1300kg TR-1 |
| Length | 9.12m |
| Wingspan | 8.50m |
| Wing area | 13.24m2 |
| Empty weight | 2400kg |
| Loaded weight | 3500kg |
| Wing Load (kg/m2) | 264 |
|
Thrust
Weight |
0.371 |
| Speed at 0m | 925km/h calculated |
| Range | 1000km calculated |
| Ceiling | 13500m calculated |
| Climb | |
| 5000m | 3.7min calculated |
| Armament | |
| Guns | 3*cannons 23mm NS-23 |
Modification of La-152, slightly larger to accommodate Lyulka TR-1 engine. Engine production was continuously delayed, and La-154 was abandoned in favor of more advanced models.
| Predecessors | Modifications |
|---|---|
| La-152 | None |
| References | Links |
|---|---|
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|
| Modified February 17, 1998 |
|
Back to Main Gate |