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

La-154 by S.A.Lavochkin

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.


PredecessorsModifications
La-152 None

ReferencesLinks
  • La-150
  • "History of aircraft construction in the USSR", Vol.2 p.349;
  • La-154, Lavochkin
  • La-154 at The Jet Genesis
  • Lavochkin aircraft at WWW.AVIATION.RU

  • Modified February 17, 1998 Back to
    Main Gate