Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
cannular |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
1 |
Bypass Ratio
—
|
Overall Pressure Ratio
—
|
Afterburner
Yes |
Pictures
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Airplanes
All data (15 fields)
- Name
- General Electric J79
- Aircraft Engine Manufacturer
- General Electric Company
- Aircraft Engine Type
- Turbojet
- Dry Weight (kg)
- 1739.527
- Diameter (mm)
- 992.124
- Length (mm)
- 5300.726
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/General_Electric_J79
- Fuel
- JP-4, JP-5
- Geared Fan
- No
- Combustion Chamber
- cannular
- Afterburner
- Yes
- Streams
- 1
- Thrust To Weight
- 3.1
- Compressor Description
- single-spool 17-stage axial compressor, with one row of variable inlet guide vanes (VIGV's) followed by 6 rows of variable stator vanes
- Turbine Description
- 3-stage