Teledyne CAE J69
J69 / J100 | |
---|---|
Teledyne-Continental J69 turbojet, Warner-Robbins Air Museum, Georgia | |
Type | Turbojet |
National origin | France/United States |
Manufacturer | Continental Aviation and Engineering / Teledyne CAE |
Major applications | BQM-34 Firebee T-37 Tweet |
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. A development of the Turbomeca 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 Teledyne CAE J100 turbojet optimized for higher altitudes
Variants
- J69
- [1]
- J69-T-9
- J69-T-19B
- J69-T-25
- J69-T-27
- J69-T-29
- J69-T-31
- J69-T-33
- 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) 17,005 lbf (75.64 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 356-29A
- (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
Wikimedia Commons has media related to Teledyne CAE J69. |
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.