Teledyne CAE J69
J69 / J100 | |
---|---|
Teledyne-Continental J69 turbojet at the Museum of Aviation, Warner Robins, Georgia | |
Type | Turbojet |
National origin | France/United States |
Manufacturer | Continental Aviation and Engineering / Teledyne CAE |
Major applications | BQM-34 Firebee T-37 Tweet Ryan Model 147 |
Developed from | Turbomeca Marboré |
The Teledyne CAE J69 was a small turbojet engine originally produced by Continental Aviation and Engineering (CAE) under license from Turbomeca. The J69 was a development of the Turbomeca Marboré II. It powered a number of U.S. drones, missiles and small aircraft. The engine was later produced by Teledyne CAE. The J69 was also developed into the Teledyne CAE J100 turbojet optimized for operation at higher altitudes.
Variants
- J69
- [1]
- J69-T-6
- J69-T-9
- J69-T-19B
- J69-T-25
- J69-T-27
- J69-T-29
- J69-T-31
- J69-T-33
- J69-T-39
- J69-T-41
- J69-T-41A
- J100-CA-100
- 2,800 lbf (12 kN) thrust
- CJ69-1025
- 1,025 lbf (4.56 kN)
- CJ69-1400
- 1,400 lbf (6.2 kN) lb thrust
- Model 352-5a
- (CJ69-T-1025) 1,025 lbf (4.56 kN) thrust
- Model 354-12
- (J69-T-27) 1,150 lbf (5.1 kN) thrust
- Model 356-7A
- (J69-T-29) 1,705 lbf (7.58 kN) thrust
- Model 356-7D
- (J69-T-29) 1,700 lbf (7.6 kN) thrust
- Model 356-8
- (J69-T-31) 1,025 lbf (4.56 kN) thrust
- Model 356-11
- (J69-T-33) 1,025 lbf (4.56 kN) thrust
- Model 356-16
- Model 356-24
- Model 356-27B
- Model 356-29A
- (J69-T-41A)
Applications
- J69
- J100
Specifications (Marboré IIC)
Data from FAA Type Certificate Data Sheet[2]
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
Related lists
References
- ↑ Flying Magazine: 27. August 1961. Missing or empty
|title=
(help) - ↑ 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. p. 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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