TEI-PD180ST
Turbodiesel Aviation Engine
TEI-PD180ST engine is developing to meet the power needs of MALE (Medium Altitude Long Endurance) class unmanned aerial vehicles.
TEI-PD180ST engine has a single stage turbocharging system, high altitude capability, low fuel consumption and a lightweight aluminum block design. With more power and less weight, it will go ahead of its competitors in the market and bring the capabilities of the platforms to a higher class.
TEI-PD180ST Technical Specifications
| Engine Configuration | Straight 4 Cylinder |
| Displacement | 2,1 Liters |
| Air Supply | Single-Stage Turbocharger |
| Fuel Supply | Common Rail |
| Take-off Power (5 minutes) | 180 HP |
| Continuous Power | 170 HP |
| High-Altitude Power (@20.000 ft.) | 170 HP |
| High-Altitude Power (@30.000 ft.) | 115 HP |
| Fuel Consumption | 220 g/kWh |
| Fuel | JP-8 or Jet-A1 |
| Dry Weight | 158 kg |
| Engine Control | Full Authority Digital Engine Control (FADEC) |
| Aircraft Configuration | Pusher and tractor |
| Propeller Control | FADEC Controlled Hydro-Mechanical Governor |
| Electrical Power Generation | 2 x 4,5 kW |
| FADEC Software and Alternator Control | DO-178C DAL-C certifiable |
