Model and type
Titan T-62T -2A1. 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. Pressure ratio 3.5:1 and air mass flow 1.6 Ib/sec.

Turbine
Radial inflow type. Turbine wheel with integral vanes and exhaust in center. Turbine inlet temperature 1,450 F (788C) and exhaust temperature 1,040 F (560 C), at 56,000 rpm.

Exhaust
Fixed area outlet at rear of turbine.

Power take-off
Reduction gearbox at front of unit. Output shaft 6,000 rpm.

Fuel system
1 Adel 70144 fuel pump 350 psi and Solar centrifugal type controls. Constant speed engine.

Ignition
High-energy capacitor discharge ignition. 1 igniter.

Lubrication
Return system. 15 psi. Integral oil tank.

Width and height
18.45in and 19.03 in

Length
26 in

Weight with gearbox
71.10 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
0.10 Ib/hr

Rating Max cont.
95shp/56,000 rpm/sea level.