Specific Fuel Consumption
30.081 g/(kN·s)
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
single annular combustion chamber |
| 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
No |
Pictures
No pictures yet for this family.
Airplanes
All data (16 fields)
- Name
- Turbomeca Piméné
- Aircraft Engine Manufacturer
- Turbomeca
- Aircraft Engine Type
- Turbojet
- Dry Weight (kg)
- 54
- Diameter (mm)
- 408
- Length (mm)
- 880
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Turbomeca_Pim%C3%A9n%C3%A9
- Fuel
- kerosene
- Geared Fan
- No
- Combustion Chamber
- single annular combustion chamber
- Afterburner
- No
- Streams
- 1
- Thrust To Weight
- 2.077
- Specific Fuel Consumption (g/(kN·s))
- 30.081
- Compressor Description
- single-stage centrifugal compressor with 14 vanes
- Turbine Description
- single-stage