Teledyne CAE J69
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
Variants
- J69
- J100
Applications
- J69
- J100
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
See also
- Related development
- Related lists
References
- 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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