Specific Fuel Consumption
16.995 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
Cannular, 10 chambers |
| 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
—
|
Overall Pressure Ratio
—
|
Afterburner
No |
Pictures
No pictures yet for this family.
Airplanes
All data (16 fields)
- Name
- Rolls-Royce Medway
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Dry Weight (kg)
- 1587.573
- Diameter (mm)
- 1066.8
- Length (mm)
- 4191
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Rolls-Royce_Medway
- Fuel
- Jet fuel
- Geared Fan
- No
- Combustion Chamber
- Cannular, 10 chambers
- Afterburner
- No
- Streams
- 2
- Thrust To Weight
- 4.94
- Specific Fuel Consumption (g/(kN·s))
- 16.995
- Compressor Description
- Axial, 6-stage LP fan, 11-stage HP
- Turbine Description
- 2-stage LP, 2-stage HP