Maximum Takeoff Thrust
72.2 kN
Specific Fuel Consumption
1841.125 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
9 chambers in can-annular arrangement, four injectors per 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
2 |
Bypass Ratio
0.97 |
Overall Pressure Ratio
—
|
Afterburner
Yes |
Pictures
No pictures yet for this family.
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All data (16 fields)
- Name
- Volvo RM8
- Aircraft Engine Manufacturer
- Svenska
- Aircraft Engine Type
- Turbofan
- Dry Weight (kg)
- 2350
- Diameter (mm)
- 1030
- Length (mm)
- 6230
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Volvo_RM8
- Geared Fan
- No
- Combustion Chamber
- 9 chambers in can-annular arrangement, four injectors per chamber
- Afterburner
- Yes
- Streams
- 2
- Bypass Ratio
- 0.97
- Maximum Takeoff Thrust (kN)
- 72.2
- Thrust To Weight
- 5.4
- Specific Fuel Consumption (g/(kN·s))
- 1841.125
- Compressor Description
- Axial flow, 3-stage fan, 3-stage LP, 7-stage HP