Product overview
The engine has a horizontally opposed, two-cylinder, two-stroke design with air cooling and high-pressure common rail technology.
Its listed applications include small vertical takeoff and landing UAVs and long-endurance compound-wing UAVs.
The published maximum altitude is 5000 m.
The listed time between overhauls is greater than 200 h.
Specifications
| Specification | Value & conditions |
|---|---|
| Maximum altitude | 5000 mPublished maximum altitude for the engine. |
| Time between overhauls | > 200 hPublished engine overhaul interval expressed as a strict greater-than threshold. |
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