Model T62T-32 Titan Gas Turbine Engine
Model and type
Titan T-62T -32. Turboshaft, 1-stage centrifugal compressor annular combustor,1-stage turbine.
Radial air intake between compressor and reduction gearbox Single-entry impeller mounted back-to-back with turbine wheel on main shaft supported in ball thrust and roller bearings. air mass flow 2.2 Ib/sec.
Radial inflow type. Turbine wheel with integral vanes and exhaust in center. Max exhaust temperature 1,180 F (638C) at 61,091 rpm.
Fixed area outlet at rear of turbine.
Reduction gearbox at front of unit. Output shaft 6,000 rpm.
1 Adel fuel pump 600 psi fuel control.
High-energy capacitor discharge ignition. 1 igniter.
Return system. 15 -65psi. Integral oil tank.
Width and height
16.81in and 21.375in
Weight with gearbox
142 Ib (dry)
Gasoline, Kerosene, or JP-4
Mil -L- 23699, L-7808
Rating Max cont.
160shp/61,091 rpm/sea level
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