THOR 260
THOR 260 was designed to give usability and versatility of use with the aim to offer more reliability and to reduce the service charges. It is the ideal engine for long distance flights, joins high performance with a smooth running.
Note: *Shipping charge is not included in this item. Please Contact us for shipping price and details.*
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DATA SHEET |
THOR 260 |
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Polini Engine |
2 stroke monocylinder |
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Cooling |
Liquid cooled |
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Bore for stroke |
76 x 62 |
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Displacement |
281 cm3 |
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Power |
36 HP |
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*Max thrust |
105 Kg with Ø 150 cm propeller |
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R.P.M. max |
8.500 |
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Cylinder |
Aluminum with Gilnisil coating |
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Compression ratio |
10:1 |
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Piston |
Two chromium plated rings mm 1 |
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Intake |
Reed valve in the crankcase |
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Carburetor |
28mm VHST Dell’Orto |
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Air filter |
Air box |
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Ignition |
Electronic with battery charger |
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Battery charger prearrangement |
Output power 40 W at 5500 RPM |
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Spark plug hood |
5k Ω resistance |
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**Fuel type |
E5 petrol or LL AV GAS-al with 2,5% synthetic oil 100% |
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*Consumption |
3,5 Lh 30 Kg of static thrust |
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Gear reduction unit |
Helical teeth in oil bath with 2,8 or 3,2 reduction ratio |
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Starter |
Electric + Flash Starter |
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Clutch |
Centrifugal in oil bath |
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Muffler |
Expansion with oval silencer |
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Engine weight |
21 kg with radiator |
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Propeller rotation |
Clockwise |
*The values have been detected on the sea level at standard atmosphere. The thrust and consumption values may vary according to the air temperature and density.
**E5 means the petrol type that can be used. E5= unleaded petrol 95 octanes up to 5% of ethanol. This symbol is shown on all the petrol pumps in Europe.