About: Curtiss R2C

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The Curtiss R2C was a racing aircraft designed for the United States Navy in 1923 by Curtiss. It was a single-seater biplane with a monocoque fuselage and staggered single-bay wings of unequal span braced with I-struts. The aircraft's advanced streamlining featured a top wing mounted directly to the top of the fuselage and surface-mounted radiators for cooling the engine. The aircraft was originally designed and built as a landplane under the Navy designation R2C-1, of which two examples were produced. One was converted into a seaplane version known as the R2C-2 the following year.

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dbo:abstract
  • The Curtiss R2C was a racing aircraft designed for the United States Navy in 1923 by Curtiss. It was a single-seater biplane with a monocoque fuselage and staggered single-bay wings of unequal span braced with I-struts. The aircraft's advanced streamlining featured a top wing mounted directly to the top of the fuselage and surface-mounted radiators for cooling the engine. The aircraft was originally designed and built as a landplane under the Navy designation R2C-1, of which two examples were produced. One was converted into a seaplane version known as the R2C-2 the following year. (en)
  • El Curtiss R2C fue un avión de carreras diseñado para la Armada de los Estados Unidos en 1923, por la estadounidense Curtiss. (es)
dbo:manufacturer
dbo:numberBuilt
  • 3 (xsd:nonNegativeInteger)
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  • 14961610 (xsd:integer)
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  • 1071317433 (xsd:integer)
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dbp:airfoil
  • Curtiss C-62 (en)
dbp:ceilingFt
  • 31800 (xsd:integer)
dbp:crew
  • 1 (xsd:integer)
dbp:emptyWeightLb
  • 1877 (xsd:integer)
dbp:eng1Hp
  • 507 (xsd:integer)
dbp:eng1Name
dbp:eng1Number
  • 1 (xsd:integer)
dbp:eng1Type
  • V-12 water-cooled piston engine (en)
dbp:firstFlight
  • 1923-09-09 (xsd:date)
dbp:grossWeightLb
  • 2071 (xsd:integer)
dbp:heightFt
  • 6 (xsd:integer)
dbp:heightIn
  • 10 (xsd:integer)
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  • 19 (xsd:integer)
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  • 8.500000 (xsd:double)
dbp:lists
  • *List of racing aircraft (en)
dbp:manufacturer
dbp:maxSpeedMph
  • 266 (xsd:integer)
dbp:maxSpeedNote
  • at sea level (en)
dbp:moreUsers
dbp:numberBuilt
  • 3 (xsd:integer)
dbp:primaryUser
dbp:primeUnits?_
  • imp (en)
dbp:propBladeNumber
  • 2 (xsd:integer)
dbp:propDiaNote
  • forged Aluminium alloy fixed-pitch propeller (en)
dbp:propName
  • Curtiss-Reed (en)
dbp:rangeMiles
  • 173 (xsd:integer)
dbp:rangeNote
  • :: cruising (en)
  • at full throttle (en)
dbp:ref
  • Curtiss Aircraft 1907–1947, United States Navy aircraft since 1911 (en)
dbp:related
  • *Curtiss R3C (en)
dbp:spanFt
  • 22 (xsd:integer)
dbp:spanIn
  • 0 (xsd:integer)
dbp:timeToAltitude
  • 216.0
dbp:type
  • Racing aircraft (en)
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dbp:wingAreaSqft
  • 148 (xsd:integer)
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • The Curtiss R2C was a racing aircraft designed for the United States Navy in 1923 by Curtiss. It was a single-seater biplane with a monocoque fuselage and staggered single-bay wings of unequal span braced with I-struts. The aircraft's advanced streamlining featured a top wing mounted directly to the top of the fuselage and surface-mounted radiators for cooling the engine. The aircraft was originally designed and built as a landplane under the Navy designation R2C-1, of which two examples were produced. One was converted into a seaplane version known as the R2C-2 the following year. (en)
  • El Curtiss R2C fue un avión de carreras diseñado para la Armada de los Estados Unidos en 1923, por la estadounidense Curtiss. (es)
rdfs:label
  • Curtiss R2C (es)
  • Curtiss R2C (en)
  • Curtiss R2C (pt)
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