Teledyne CAE J69
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
Data from: Aircraft engines of the World 1957[1]
- J69-T-1
- (Marboré I) Template:Cvt at 23,000 rpm.[2]
- J69-T-3
- Template:Cvt at 22,500 rpm for take-off.[2]
- J69-T-6
- J69-T-9
- J69-T-17
- J69-T-19
- J69-T-19A
- J69-T-19B
- J69-T-23
- J69-T-25
- J69-T-27
- J69-T-29
- J69-T-31
- J69-T-33
- J69-T-39
- J69-T-41
- J69-T-41A
- J69-T-406
- J100-CA-100
- Script error: No such module "convert". thrust
- CJ69-1025
- Script error: No such module "convert".
- CJ69-1400
- Script error: No such module "convert". lb thrust
- Model 352
- Model 352A
- Model 352-5a
- (CJ69-T-1025) Script error: No such module "convert". thrust
- Model 354-12
- (J69-T-27) Script error: No such module "convert". thrust
- Model 356-7A
- (J69-T-29) Script error: No such module "convert". thrust
- Model 356-7D
- (J69-T-29) Script error: No such module "convert". thrust
- Model 356-8
- (J69-T-31) Script error: No such module "convert". thrust
- Model 356-11
- (J69-T-33) Script error: No such module "convert". 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[3]
General characteristics
- Type: turbojet
- Length: Script error: No such module "convert".
- Diameter: Script error: No such module "convert".
- Dry weight: Script error: No such module "convert".
Components
- Compressor: single stage centrifugal
- Combustors: single annular combustion chamber
- Turbine: single stage
Performance
- Maximum thrust: Script error: No such module "convert". at 22,600 rpm
- Turbine inlet temperature: Script error: No such module "convert".
- Thrust-to-weight ratio: 2.458
See also
Related development
Related lists
References
<templatestyles src="Reflist/styles.css" />
- ↑ Script error: No such module "citation/CS1".
- ↑ a b Script error: No such module "citation/CS1".
- ↑ FAA Type Certificate Data Sheet Script error: No such module "webarchive". Retrieved: 2 November 2008
Script error: No such module "Check for unknown parameters".
- Script error: No such module "citation/CS1".
- Script error: No such module "citation/CS1".
External links
Script error: No such module "Side box".
- Aircraft fitted with MARBORE II or VI Script error: No such module "webarchive".
Template:CAE/TTE aeroengines Script error: No such module "Navbox".