Solar T62

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Solar T62
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Solar T62T-27 engine used as auxiliary power unit (APU)
Role Small gas turbineTemplate:Short description
National origin United States
Manufacturer Solar Turbines
First flight 1950s
Primary user United States Army

The Solar T62 Titan is an American gas turbine engine used mainly as an aircraft auxiliary power unit (APU), conventional power generator, turboprop engine for fixed-wing aircraft or turboshaft engine for helicopters. A new turbine version was developed as the Solar T66.

Variants

T62 Titan
The direct drive main production version.
T62T-2
Script error: No such module "convert". at 56,700 turbine rpm for Boeing-Vertol CH-47A Chinook helicopters.[1]
T62T-2A
Script error: No such module "convert". at 56,700 turbine rpm for Boeing-Vertol CH-47B / C Chinook helicopters.[1]
T62T-11
Script error: No such module "convert". at 56,700 turbine rpm for Boeing-Vertol CH-46A Sea Knight helicopters.[1]
T62T-12
Script error: No such module "convert". at 61,240 turbine rpm
T62T-16 / -16A1
Script error: No such module "convert". for Sikorsky CH-3, Sikorsky SH-3 and Sikorsky CH-54A Skycrane helicopters at 56,700 turbine rpm, with 8,000 and 8,100 rpm outputs.[1]
T62T-25
Turboshaft - Script error: No such module "convert". at 56,700 turbine rpm
T62T-27
Turboshaft - Script error: No such module "convert". at 61,250 turbine rpm, with 1x 8,000 and 1x 8,216 rpm outputs.[1]
T62T-29
Turboshaft - Script error: No such module "convert". at 56,700 turbine rpm, for Lockheed Jetstar and Pan American Falcon business Jets at 56,700 turbine rpm, with 1x 8,000 and 1x 8,100 rpm outputs.[1]
T62T-32A
Script error: No such module "convert". at 61,250 rpm. Military Ground Power Unit (GPU) often used by US Navy and Air Force.
T62T-39
T66
A free power turbine version for the US military.

Applications

Auxiliary Power Unit
Turboshaft
Turboprop

Specifications

Data from Bennett[2]

General characteristics

  • Type: Turboshaft
  • Length: Script error: No such module "convert".
  • Diameter: Script error: No such module "convert".
  • Dry weight: Script error: No such module "convert".

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: Script error: No such module "convert".
  • Power-to-weight ratio: Script error: No such module "convert".

Notes

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External links

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