| Ardiden 1H ✕ | |
|---|---|
| Family | Ardiden |
| Aircraft Engine Manufacturer | Safran Helicopter Engines |
| Aircraft Engine Type | Turboshaft |
| Comment | Drhuv, LCH |
| Dry Weight (kg) | 205 |
| Length (mm) | 1250 |
| Height (mm) | 649 |
| Width (mm) | 519 |
| Control System | FADEC Dual Channel |
| Certification | 2007-12-20 |
| Modules | 3 |
| Time Between Overhaul (h) | 3000 |
| Fuel | Jet-A1 |
| LP Compressor Stages | 0 |
| IP Compressor Stages | 0 |
| HP Compressor Stages | 2 |
| HP Compressor Technology | 2 centrifugal |
| Combustion Chamber | Annular reverse flow |
| HP Turbine Stages | 1 |
| HP Turbine Technology | axial |
| IP Turbine Stages | 0 |
| LP Turbine Stages | 2 |
| LP Turbine Technology | axial |
| Maximum Takeoff Power (kW) | 938 |
| Maximum 30min Power (kW) | 938 |
| Maximum Continuous Power (kW) | 801 |
| OEI30sec Power (kW) | 1108 |
| OEI2min Power (kW) | 975 |
| OEI Continuous Power (kW) | 931 |
| Output Take Off Speed (rpm) | 6000 |
| Output Clockwise Rotation | Yes |