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T55-L-712
✕
|
| Family |
T55 |
| Aircraft Engine Manufacturer |
Honeywell |
| Aircraft Engine Type |
Turboshaft |
| Comment |
3,750 shp ( 2,798 kW) |
| Dry Weight (kg) |
377 |
| Length (mm) |
1196.3 |
| Height (mm) |
615.9 |
| Width (mm) |
615.9 |
| Time Between Overhaul (h) |
3000 |
| Fuel |
Jet-A1 |
| LP Compressor Stages |
0 |
| IP Compressor Stages |
0 |
| HP Compressor Stages |
8 |
| HP Compressor Technology |
6 axial, 1 centrifugal |
| Combustion Chamber |
Annular reverse flow |
| HP Turbine Stages |
2 |
| HP Turbine Technology |
axial |
| IP Turbine Stages |
0 |
| LP Turbine Stages |
2 |
| LP Turbine Technology |
axial |
| Overall Pressure Ratio |
9.32 |
| T4 Take Off (°C) |
815 |
| Output Take Off Speed (rpm) |
14750 |
| Output Clockwise Rotation |
Yes |