The Solar T62 Titan is an American gas-turbine engine used mainly as a helicopter auxiliary power unit (APU), ground power generator or helicopter power-plant. A free power turbine version was developed as the Solar T66.
- T62 Titan
- The direct drive main production version.
- 80 hp (60 kW) @ 56,700 turbine rpm for Boeing-Vertol CH-47A Chinook helicopters.
- 95 hp (71 kW) @ 56,700 turbine rpm for Boeing-Vertol CH-47B / C Chinook helicopters.
- 80 hp (60 kW) @ 56,700 turbine rpm for Boeing-Vertol CH-46A Sea Knight helicopters.
- 105 hp (78 kW) @ 61,240 turbine rpm
- T62T-16 / -16A1
- 95 hp (71 kW) for Sikorsky CH-3, Sikorsky SH-3 and Sikorsky CH-54A Skycrane helicopters @ 56,700 turbine rpm, with 8,000 and 8,100 rpm outputs.
- turboshaft - 80 hp (60 kW) @ 56,700 turbine rpm
- turboshaft - 150 hp (110 kW) @ 61,250 turbine rpm, with 1x 8,000 and 1x 8,216 rpm outputs.
- turboshaft - 95 hp (71 kW) @ 56,700 turbine rpm, for Lockheed Jetstar and Pan American Falcon business Jets @ 56,700 turbine rpm, with 1x 8,000 and 1x 8,100 rpm outputs.
- 150 hp (110 kW) @ 61,250 rpm. Military Ground Power Unit (GPU) often used by US Navy and Air Force.
- A free power turbine version for the US military.
- Auxiliary Power Unit
Data from Bennett
- Type: Turboshaft
- Length: 33.41 in (84.86 cm)
- Diameter: 21.375 in (54.293 cm)
- Dry weight: 142 lb (64 kg) lb
- 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
- Maximum power output: 60 to 150 hp (45 to 112 kW)
- Power-to-weight ratio: 0.42 to 1.06 hp/lb (0.69 to 1.74 kW/kg)