Maximum Takeoff Thrust
71.6 kN
Specific Fuel Consumption
17.816 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
Annular |
| 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
2 |
Bypass Ratio
4.4 |
Overall Pressure Ratio
—
|
Afterburner
No |
Pictures
No pictures yet for this family.
Similar reaction turbines
All data (18 fields)
- Name
- PowerJet SaM146
- Aircraft Engine Manufacturer
- PowerJet
- Aircraft Engine Type
- Turbofan
- Dry Weight (kg)
- 2260
- Diameter (mm)
- 1220
- Length (mm)
- 3590
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/PowerJet_SaM146
- Fuel
- Jet A, Jet A-1, TS-1, RP (*)
- Geared Fan
- No
- Combustion Chamber
- Annular
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.4
- Maximum Takeoff Thrust (kN)
- 71.6
- Thrust To Weight
- 3.5
- Specific Fuel Consumption (g/(kN·s))
- 17.816
- Compressor Description
- 1 stage fan, 3-stage low pressure, 6-stage high pressure axial
- Turbine Description
- 1-stage high pressure, 3-stage low pressure