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.

Variants

J69

J100

Applications

J69

• Cessna T-37 Tweet
• Radioplane Q-1
• Ryan BQM-34 Firebee
• Temco TT Pinto

J100

• Ryan Model 147T

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)

Components

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

Performance

• Maximum thrust: 880 lbf (3.91 kN) at 22,600 rpm
• Turbine inlet temperature: 650 C
• Thrust-to-weight ratio: 2.458 lbf/lb (0.024 kN/kg)

See also

Related development

• Turbomeca Marboré
  

Related lists

• List of aircraft engines
  

References

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

• Aircraft fited with MARBORE II or VI