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 main 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