About: Zenoah G-50

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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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dbo:abstract
  • The Zenoah G-50 is a twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine, designed for use on ultralight aircraft. (en)
dbo:wikiPageID
  • 25550212 (xsd:integer)
dbo:wikiPageLength
  • 4574 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1000266561 (xsd:integer)
dbo:wikiPageWikiLink
dbp:compression
  • 6.500000 (xsd:double)
dbp:coolingsystem
  • free air (en)
dbp:displacement
  • 484.0
dbp:fueltype
dbp:manufacturer
  • Zenoah (en)
dbp:nationalOrigin
dbp:oilsystem
  • pre-mixed (en)
dbp:power
  • at 5800 rpm (en)
dbp:reductionGear
  • 2.100000 (xsd:double)
dbp:ref
  • Cliche & Tennessee Propellers (en)
dbp:type
  • Twin cylinder two-stroke aircraft engine (en)
  • Two cylinder, two-stroke aircraft engine (en)
dbp:unitCost
  • 2990.0
dbp:valvetrain
  • piston ported (en)
dbp:weight
  • equipped with reduction drive, electric start and muffler (en)
dbp:wikiPageUsesTemplate
dcterms:subject
rdf:type
rdfs:comment
  • The Zenoah G-50 is a twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine, designed for use on ultralight aircraft. (en)
rdfs:label
  • Zenoah G-50 (en)
owl:sameAs
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