| Aircraft Engine Manufacturer |
Bristol Engine Company (Bristol) |
| Aircraft Engine Type |
Turbofan |
| Dry Weight (kg) |
1796.226 |
| Diameter (mm) |
1219.2 |
| Length (mm) |
3479.8 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Rolls-Royce_Pegasus |
| Geared Fan |
No |
| Combustion Chamber |
Annular |
| Afterburner |
No |
| Streams |
2 |
| Maximum Takeoff Thrust (kN) |
106 |
| Thrust To Weight |
6 |
| Specific Fuel Consumption (g/(kN·s)) |
21.527 |
| Compressor Description |
3-stage low pressure, 8-stage high pressure axial flow |
| Turbine Description |
2-stage high pressure, 2-stage low pressure |