Turbomeca Palas
The Turbomeca Palas is a diminutive centrifugal flow turbojet engine used to power light aircraft. It was designed in 1950 by the French manufacturer Société Turbomeca, and was also produced under licence by Blackburn and General Aircraft in the United Kingdom and Teledyne Continental Motors in the United States.
Applications
Specifications
General characteristics
- Type: turbojet
- Length: 1.2 m (47.25 in)
- Diameter: 405 mm (16 in)
- Dry weight: 72 kg (159 lb)
Components
- Compressor: single-stage centrifugal
- Combustors: annular with rotary fuel injection
- Turbine: single-stage with 24 or 25 blades
- Fuel type: Jet A1
Performance
See also
- Related lists
References
External links
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