Hirth F-36
http://dbpedia.org/resource/Hirth_F-36 an entity of type: MeanOfTransportation
The Hirth F-36 is a single-cylinder, two-stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and ultralight trikes. It is noted for its extremely small equipped weight of 28 lb (13 kg) including exhaust system, reduction drive and carburetor. It is manufactured by Hirth of Germany. The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth.
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Hirth F-36
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25506266
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1068083304
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at 6000 rpm
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Recreational Power Engineering
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Single cylinder, two-stroke, aircraft engine
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Single-cylinder two-stroke aircraft engine
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with reduction drive, exhaust system and recoil start
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The Hirth F-36 is a single-cylinder, two-stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and ultralight trikes. It is noted for its extremely small equipped weight of 28 lb (13 kg) including exhaust system, reduction drive and carburetor. It is manufactured by Hirth of Germany. The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth.
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10.6
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free air
<cubicCentimetre>
208.0
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1
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Minimum of unleaded 93 octane auto fuel
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50
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four element cog belt with ratios of 1.8:1, 2.0:1 or 2.5:1 available
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5289