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Solar
Model T62T-2A1 Titan Gas Turbine Engine |
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Model and type
Titan T-62T -2A1. Turboshaft, 1-stage centrifugal compressor, annular combustor, 1-stage
turbine.
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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. Pressure ratio 3.5:1 and air mass flow 1.6 Ib/sec.
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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.
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Exhaust
Fixed area outlet at rear of turbine.
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Power take-off
Reduction gearbox at front of unit. Output shaft 6,000 rpm.
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Fuel system
1 Adel 70144 fuel pump 350 psi and Solar centrifugal type controls. Constant speed engine. |
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Ignition
High-energy capacitor discharge ignition. 1 igniter. |
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Lubrication
Return system. 15 psi. Integral oil tank. |
Width and height
18.45in and 19.03 in |
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Length
26 in |
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Weight with gearbox
71.10 Ib (dry) |
Power weight
1.25 shp/Ib |
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Fuel spec
Gasoline, Kerosene, or Jp-4 |
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Fuel consumption
1.3 Ib/shp-hr |
Oil spec
Mil -L- 23699, L-7808 |
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Oil Consumption
0.10 Ib/hr |
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Rating Max cont.
95shp/56,000 rpm/sea level. |
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