Technical data
Type La-150F
Function Experimental fighter
Year 1947
Crew 1
Engines 1*1100kg RD-10F
Length 9.42m
Wingspan 8.50m
Wing area 13.24m2
Loaded weight 3340kg
Wing Load (kg/m2) 252
Thrust
Weight
0.323
Speed at 0m 950km/h
Speed at 5000m900km/h
Flight Endurance 48min
Ceiling 13000m
Climb
5000m 4.0min
Armament
Guns 2*cannons 23mm NS-23

La-150F by S.A.Lavochkin

"History of aircraft construction in the USSR", Vol.2 p 348

Modification of the La-150 for afterburning RD-10F engine. Wing area was increased, and its tips were tilted down by 30°

Flight tested in July-September 1947.


PredecessorsModifications
La-150M La-152

ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.2 p.349;
  • La-150

  • Created February 17, 1998 Back to
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