|Wing Load (kg/m2)||275|
|Speed at 0m||760km/h|
|Speed at 5000m||805km/h|
|Guns||2*cannons 23mm NS-23|
Pre-production series development of the La-150. Fuel tanks capacity was increased, tailfin enlarged. Curved windscreen was replaced by the flat one (more technological). As a result of all those changes, flight weight increased by 300-400kg. Aircraft still was unable to fulfill all requirements (TTKh).
At the same time handling problems were fixed. Small pre-production butch of the La-150M was sent to fighter regiments for evaluation. Regiment tests continued until September 1947. La-150M was not accepted by military and remained an experimental aircraft.
La-150 Type 3
|Created February 17, 1998||Back to|