The Light Helicopter Turbine Engine Company T800 is a turboshaft engine for rotary wing applications. It is produced by the LHTEC, a joint venture between Rolls-Royce and Honeywell. The commercial and export version is the CTS800. The engine was primarily developed for the United States Army's RAH-66 Comanche armed reconnaissance helicopter, but has found use in other applications.
Applications
Specifications
| Engine |
Power (shp) |
SFC (lb/hr/shp) |
Overall Pressure Ratio |
Mass Flow (lb/s) |
Basic Engine Weight (lb) |
Length (in) |
|---|
| T800-LHT-801 |
1563 | ~0.459 | 15 | 10 | 315 | 31.5 |
| CTS800-4N |
1362 | ? | 15 | 7.2 | 374 | 48 |
T800-LHT-801
Data from [citation needed]
General characteristics
- Type: turboshaft
- Length: 31.5 inches (0.80 m)
- Diameter:
- Dry weight: 315 pounds (143 kg)
Components
- Compressor: 2CFHP
- Turbine: 2HP, 2PT
Performance
See also
References
External links
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