LHTEC T800
| T800 / CTS800 | |
|---|---|
 | |
| An AgustaWestland AW159 Lynx Wildcat illustrating the installation of the LHTEC T800 turboshaft engines. | |
| Type | Turboshaft |
| National origin | United States |
| Manufacturer | LHTEC |
| Major applications | AgustaWestland AW159 RAH-66 Comanche TAI/AgustaWestland T-129 |
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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 cancelled RAH-66 Comanche armed reconnaissance helicopter, but has found use in other applications.
Applications
- AgustaWestland Super Lynx 300 (CTS800-4N)
- AgustaWestland AW159 Wildcat (CTS800-4N)
- Ayres LM200 Loadmaster (LHTEC CTP800-4T) (aircraft not built)
- Boeing-Sikorsky RAH-66 Comanche (cancelled)
- ShinMaywa US-2 (CTS800-4K) - boundary layer compressor drive
- Sikorsky X2 (T800-LHT-801)
- TAI/AgustaWestland T129 (CTS800-4A)
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
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
- Maximum power output: 1,563 shp (1,166 kW)
- Specific fuel consumption: ~0.459 lb/shp/hr
- Power-to-weight ratio:
See also
References
External links
This article is issued from Wikipedia - version of the 10/26/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.