Solar T62
From Wikipedia, the free encyclopedia
The Solar T62 Titan is an American gas-turbine engine used mainly as a helicopter Auxiliary Power Unit, ground power generator or helicopter power-plant. A free power turbine version was developed as the Solar T66.
Variants
- T62 Titan
- The direct drive mainproduction version.
- T66
- A free power turbine version for the US military.
Applications
- Auxiliary Power Unit
- Boeing CH-46 Sea Knight
- Boeing CH-47 Chinook
- Sikorsky CH-54 Tarhe
- Turboshaft
- Alpi Syton AH 130
- AvioTecnica ES-101 Raven
- Eagle Helicycle
- Famà Kiss 209
- Mosquito Aviation XE
- RotorWay Exec 162F (upgrades)
- Ultrasport496 (upgrades)
- Gyrodyne RON Rotorcycle
- Turboprop
Specifications
Data from Bennett[1]
General characteristics
- Type: Turboshaft
- Length: 33.41 in (84.86 cm)
- Diameter: 21.375 in (54.293 cm)
- Dry weight: 142 lb (64 kg) lb
Components
- Compressor: Centrifugal Impeller
- Combustors: Annular reverse flow with six burners
- Turbine: Radial inflow impeller
- Fuel type: JP-4 / JP-5 / JP-8
- Oil system: Wet sump
Performance
- Maximum power output: 60 to 150 hp (45 to 112 kW)
- Power-to-weight ratio:
Notes
- ↑ "Solar T62 Titan Gas Turbine". Ian Bennett. Retrieved 2010-01-24.
External links
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