Teledyne CAE J69

Teledyne CAE J69
J69 / J100
J69 turbojet, a licensed version of the Marboré engine series
Type Turbojet
National origin France/United States
Manufacturer CAE/Teledyne CAE
Major applications BQM-34 Firebee
T-37 Tweet
Developed from Turbomeca Marboré

The Teledyne CAE J69 was a small turbojet engine produced by Continental Aviation and Engineering (CAE) under license from Turbomeca. A development of the Marboré II, the J69 powered a number of US drones, missiles and small aircraft. Later produced by Teledyne CAE, the J69 was also developed into the J100 turbojet optimized for higher altitudes

The J69 of a TT-1 Pinto.






Specifications (Marboré IIC)

Data from FAA Type Certificate Data Sheet[1]

General characteristics

  • Type: Turbojet
  • Length: 61.7 in (156.7 cm)
  • Diameter: 24.9 in (63.2 cm)
  • Dry weight: 358 lb (162.4 kg)


  • Compressor: Single stage centrifugal
  • Combustors: Single annular combustion chamber
  • Turbine: Single stage


See also

Related development

Related lists


  1. ^ FAA Type Certificate Data Sheet Retrieved: 2 November 2008
  • Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. pp. 79. ISBN 0-7509-4479-X. 
  • Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1. 

External links

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