The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft.

An enlargement of the Turbomeca Piméné, the Palas was designed in 1950 by the French manufacturer Société Turbomeca,[1] and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States as the Continental Model 320.

Data from Aircraft engines of the World 1953 [2] Related lists