About: Zenoah G-25

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The Zenoah G-25 is a single cylinder, two stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft

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dbo:abstract
  • The Zenoah G-25 is a single cylinder, two stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft (en)
dbo:wikiPageID
  • 25549914 (xsd:integer)
dbo:wikiPageLength
  • 4663 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 998848825 (xsd:integer)
dbo:wikiPageWikiLink
dbp:compression
  • 6.500000 (xsd:double)
dbp:coolingsystem
  • free air (en)
dbp:displacement
  • 242.0
dbp:fueltype
dbp:manufacturer
  • Zenoah (en)
dbp:nationalOrigin
dbp:oilsystem
  • pre-mixed (en)
dbp:power
  • at 6600 rpm (en)
dbp:reductionGear
  • 2.500000 (xsd:double)
dbp:ref
  • Cliche & Tennessee Propellers (en)
dbp:type
  • Single cylinder two-stroke aircraft engine (en)
  • Single cylinder, two-stroke aircraft engine (en)
dbp:unitCost
  • 2172.0
dbp:valvetrain
  • piston ported (en)
dbp:wikiPageUsesTemplate
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • The Zenoah G-25 is a single cylinder, two stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft (en)
rdfs:label
  • Zenoah G-25 (en)
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