Turbomeca Palas

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

• Caproni Trento F.5
• Curtiss C-46 Commando (two under the fuselage, the first flight in October 1952)
• Curtiss Commando C-46F (2 under the wings)
• CVV-6 Canguro Palas
• Douglas DC-3 (as a booster engine)
• Fouga CM-8 R9.8 Cyclope
• Fouga CM-8 R8.3 Midget
• Fouga CM.130
• Ikarus 451
• Ikarus S451M
• Ikarus 452M
• Mantelli AM-12
• Miles Sparrowjet
• Payen Pa 49
• Short SB.4 Sherpa
• SIPA S.200 Minijet
• SIPA S.300
• Somers-Kendall SK-1
• Sud-Ouest Bretagne

Specifications

Data from ^{[citation needed]}

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

• Maximum thrust: 1.6 kN (353 lbf)
• Overall pressure ratio: 3.95:1
• Turbine inlet temperature: 700°C
• Fuel consumption: 0.117 kg N^-1 h^-1 (1.15 lb lbf^-1 h^-1 )
• Thrust-to-weight ratio: 22.2 N kg^-1 (2.26 lbf lb^-1)

See also

Related lists

• List of aircraft engines

References

Notes

Bibliography

External links

Wikimedia Commons has media related to Turbomeca Palas.

• Palas at Minijets.org