TEI-PD200
Turbodiesel Aviation Engine
Developed by TEI to meet the high power requirements of Medium Altitude Long Endurance (MALE) class unmanned aerial vehicles during takeoff, the TEI-PD200 Turbodiesel Aviation Engine delivers a power output of 197 HP (±2).
Featuring a two-stage series turbocharging system, the TEI-PD200 surpasses its competitors with its superior altitude performance and fuel efficiency. The engine operates on JP-8, JP-5, or Jet-A1 fuels and has a dry weight of 162 kg. Designed in accordance with civil aviation standards, the TEI-PD200 is equipped with a Redundant Engine Control System developed and manufactured by TEI. The engine has a service ceiling of 45,000 ft.
The TEI-PD200 engine continues its flights with the Bayraktar TB3 platform.
TEI-PD200 Technical Specifications
| Displacement | 2.1 L |
| Engine Configuration | Straight 4 Cylinder |
| Fuel Supply | Common Rail Diesel Injection |
| Air Induction | Two-Stage Turbocharging |
| Maximum Power | 197 HP (±2) |
| Maximum Continuous Power | 172 HP (±2) |
| Dry Weight | 162 kg |
| Engine Lifespan | 3600 hours |
| Engine Depot-Level Maintenance | 1200 hours |
| Engine Cooling | Water Cooled |
| Fuel Options | JP-8, JET-A1, JP-5, and EN 590 |
| BSFC (@MSL) | 207 g/kWh (±3) |
| Electrical Power | 9 kW (2 x 4,5 kW) |
| Altitude Power (@20,000 ft) | 170 HP |
| Altitude Power (@30,000 ft) | 130 HP |
| Altitude Power (@40,000 ft) | 90 HP |
| Critical Altitude | 20,000 ft |
| Maximum Altitude | 45,000 ft |
| Aircraft Configuration | Tractor or Pusher Compatible |
| Engine Control | Redundant ECU (FADEC) |
| FADEC Software | DO-178C DAL-C Certifiable |
| Alternator Control | DO-178C DAL-C Certifiable |