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Model T62T-32 Titan Gas Turbine Engine  
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Model T62T-32 Titan Gas Turbine Engine


To view T62T-32 operational package click here

Model and type
Titan T-62T -32. Turboshaft, 1-stage centrifugal compressor annular combustor,1-stage turbine.

Compressor
Radial air intake between compressor and reduction gearbox Single-entry impeller mounted back-to-back with turbine wheel on home shaft supported in ball thrust and roller bearings. air mass flow 2.2 Ib/sec. 

Turbine
Radial inflow type. Turbine wheel with integral vanes and exhaust in center. Max exhaust temperature 1,180 F (638C) at 61,091 rpm. 

Exhaust
Fixed area outlet at rear of turbine.

Power outlet
Reduction gearbox at front of unit. Output shaft 6,000 rpm.



Fuel system
1 Adel fuel pump 600 psi fuel control.
Ignition
High-energy capacitor discharge ignition. 1 igniter.
Lubrication
Return system. 15 -65psi. Integral oil tank.


Width and height
16.81in and 21.375in


 Length
33.41 in


Weight with gearbox
142 Ib (dry)


Power weight
1.25 shp/Ib


Fuel spec
Gasoline, Kerosene, or JP-4


Fuel consumption
1.3 Ib/shp/hr


Oil spec
Mil -L- 23699, L-7808


Oil Consumption
0.02 phr


Rating Max cont. 160shp/61,091 rpm/sea level


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