Lycoming T53
From Wikipedia, the free encyclopedia
The Lycoming T53 is a turboshaft engine used on American helicopters and fixed-wing aircraft (in turboprop form), since the 1950s.
[edit] Variants
- T53-L-11: 825 hp (615 kW)
- T53-L-701: 1,400 hp (1044 kW)
[edit] Specifications (T53-L-701)
General characteristics
- Type: Turboshaft
- Length:
- Diameter:
- Dry weight:
Components
- Compressor: 5-stage axial compressor and 1-stage centrifugal compressor
Performance
- Power output: 1,400 shp (1,044 kW)
- Power-to-weight ratio: