Zenoah G-50
http://dbpedia.org/resource/Zenoah_G-50 an entity of type: WikicatTwo-strokeAircraftPistonEngines
The Zenoah G-50 is a twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine, designed for use on ultralight aircraft.
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Zenoah G-50
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25550212
xsd:integer
1000266561
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piston ported
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Zenoah
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at 5800 rpm
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Cliche & Tennessee Propellers
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Twin cylinder two-stroke aircraft engine
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Two cylinder, two-stroke aircraft engine
<usDollar>
2990.0
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equipped with reduction drive, electric start and muffler
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The Zenoah G-50 is a twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine, designed for use on ultralight aircraft.
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6.5
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free air
<cubicCentimetre>
484.0
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pre-mixed
xsd:double
2.1
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4574