Turbomeca Palas

Palas
Sectioned Turbomeca Palas
Type Turbojet
National origin France
Manufacturer Turbomeca
Major applications Miles Sparrowjet
Short SB.4 Sherpa
Developed from Turbomeca Piméné

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.

Applications

Specifications

Data from

General characteristics

Components

Performance

See also


Related lists

References

Notes
  1. Gunston 1989, p. 169.
Bibliography
  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

External links

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