ROTO 35 FS AL
Single cylinder four-stroke air-cooled petrol internal combustion engine
ROTO 35 FS AL is suitable for UAV projects within the range of 4 meters and weight up to 25 kg.
ROTO 35 FS AL is suitable for UAV projects within the range of 4 meters and weight up to 25 kg.
| Engine capacity | 35 ccm |
| Fuel consumption | 290-510 g/h |
| Engine output | 1,8 HP (1750 Watts) |
| Engine weight | from 1740 g |
| Arrangement of the engine | single cylinder |
| Cooling | air-cooled |
| Lubrication | petrol 95 oct. + 2% oil |
| Speed | 1400 – 6500 rpm |
| Speed with alternator | 3200 – 6500 rpm (limiter) |
| Ceiling | 3000 metres above sea level |
| Fuel system | Carburettor (+Altimeter unit) |
| Flight modes (lifetime) | 200+ hours if TBO is kept |
Cannot be used as a starter.
| Alternator 300W | Alternator 600W | |
|---|---|---|
| PMG ( Permanent Magnet Generator) | 3 phase output | |
| NdFeB magnets | ||
| Voltage curve | 14V/1000RPM (possibility of rewinding according to client) | |
| Diameter | 101mm | |
| Thickness | 22mm | 25mm |
| Weight | 450g | 550g |
| Out. Power at 3000RPM | 300W | 430W |
| Out. Power at 6000RPM | 600W | 960W |
| Cooling | forced by air flow | |
| Resistance | to fuel, oil, water, mechanical stress | |
| Operating temperature | -30°C to 120°C | |
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Can be used as a starter.
In the span of 5-60 volts with a number of outputs and voltage according to customer requirements.
