| Solar T62 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Solar |
| Aircraft Engine Type | Turboshaft |
| Dry Weight (kg) | 64.4101 |
| Diameter (mm) | 542.925 |
| Length (mm) | 848.614 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Solar_T62 |
| Fuel | JP-4 / JP-5 / JP-8 |
| Combustion Chamber | Annular reverse flow with six burners |
| Maximum Takeoff Power (kW) | 44.742 |
| Power To Weight (kW/kg) | 0.69 |
| Compressor Description | Centrifugal Impeller |
| Turbine Description | Radial inflow impeller |