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T53-L-13
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|
| Family |
T53 |
| Aircraft Engine Manufacturer |
Honeywell |
| Aircraft Engine Type |
Turboshaft |
| Dry Weight (kg) |
247 |
| Length (mm) |
1209 |
| Height (mm) |
622 |
| Width (mm) |
622 |
| Time Between Overhaul (h) |
2400 |
| Fuel |
Jet-A1 |
| LP Compressor Stages |
0 |
| IP Compressor Stages |
0 |
| HP Compressor Stages |
6 |
| HP Compressor Technology |
5 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 |
7.4 |
| Output Clockwise Rotation |
Yes |