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The Renault 50/60 hp aircraft engines were a series of air cooled 90° V-8 engines with a bore and stroke of 90 mm × 120 mm (3.5 in × 4.7 in) built by the French Renault company in the years from 1908 to about 1911.

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  • The Renault 50/60 hp aircraft engines were a series of air cooled 90° V-8 engines with a bore and stroke of 90 mm × 120 mm (3.5 in × 4.7 in) built by the French Renault company in the years from 1908 to about 1911. (en)
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  • 12198 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1087266626 (xsd:integer)
dbo:wikiPageWikiLink
dbp:coolingsystem
  • Air-cooled (en)
dbp:developedInto
dbp:firstRun
  • c.1908 (en)
dbp:lists
  • *List of aircraft engines (en)
dbp:manufacturer
dbp:nationalOrigin
  • France (en)
dbp:power
  • at 1,800 rpm (en)
dbp:reductionGear
  • 0.500000 (xsd:double)
dbp:ref
  • Angle (en)
dbp:related
  • *Renault 70 hp (en)
dbp:type
dbp:wikiPageUsesTemplate
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rdfs:comment
  • The Renault 50/60 hp aircraft engines were a series of air cooled 90° V-8 engines with a bore and stroke of 90 mm × 120 mm (3.5 in × 4.7 in) built by the French Renault company in the years from 1908 to about 1911. (en)
rdfs:label
  • Renault 50/60 hp (en)
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