About: THK-5

An Entity of Type: mean of transportation, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The THK-5 was a twin-engine aircraft designed by Stanisław Rogalski and built in Turkey in 1945 as an air ambulance. It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A and three examples of an improved version of the 5A designated THK-10. A single example of the type was exported, sold to Denmark.

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dbo:abstract
  • The THK-5 was a twin-engine aircraft designed by Stanisław Rogalski and built in Turkey in 1945 as an air ambulance. It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A and three examples of an improved version of the 5A designated THK-10. A single example of the type was exported, sold to Denmark. When THK was taken over by MKEK, this was one of the designs selected for further work. However, although the designation MKEK-5 was allocated, nothing further came of this. (en)
  • Le THK-5 était un avion de transport civil construit en Turquie durant les années 1940. (fr)
dbo:manufacturer
dbo:numberBuilt
  • 13 (xsd:nonNegativeInteger)
dbo:wikiPageID
  • 20005061 (xsd:integer)
dbo:wikiPageLength
  • 5128 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1102936261 (xsd:integer)
dbo:wikiPageWikiLink
dbp:airfoil
  • root: NACA 23018; tip: NACA 23012 (en)
dbp:aspectRatio
  • 7.650000 (xsd:double)
dbp:capacity
  • 4 (xsd:integer)
dbp:ceilingM
  • 4000 (xsd:integer)
dbp:climbRateMs
  • 3.200000 (xsd:double)
dbp:crew
  • 2 (xsd:integer)
dbp:cruiseSpeedKmh
  • 160 (xsd:integer)
dbp:cruiseSpeedNote
  • *Landing speed: (en)
dbp:emptyWeightKg
  • 1450 (xsd:integer)
dbp:eng1Hp
  • 130 (xsd:integer)
dbp:eng1Name
dbp:eng1Number
  • 2 (xsd:integer)
dbp:eng1Type
  • 4 (xsd:integer)
dbp:firstFlight
  • 1945 (xsd:integer)
dbp:grossWeightKg
  • 1930 (xsd:integer)
dbp:heightM
  • 3.100000 (xsd:double)
dbp:lengthM
  • 10 (xsd:integer)
dbp:manufacturer
dbp:maxSpeedKmh
  • 205 (xsd:integer)
dbp:maxSpeedNote
  • at sea level (en)
dbp:morePerformance
  • *Take-off run: *Landing run: (en)
dbp:nationalOrigin
  • Turkey (en)
dbp:numberBuilt
  • 13 (xsd:integer)
dbp:primeUnits?_
  • met (en)
dbp:propBladeNumber
  • 2 (xsd:integer)
dbp:propName
  • MKEK wooden fixed-pitch propellers (en)
dbp:rangeKm
  • 650 (xsd:integer)
dbp:ref
  • Jane's All the World's Aircraft 1958-59, Jane's all the World's Aircraft 1949-50 (en)
dbp:spanM
  • 14.640000 (xsd:double)
dbp:stallSpeedKmh
  • 100 (xsd:integer)
dbp:stallSpeedNote
  • with flaps (en)
dbp:type
  • Air ambulance and light transport (en)
dbp:wikiPageUsesTemplate
dbp:wingAreaSqm
  • 28 (xsd:integer)
dbp:wingLoadingKg/m
  • 64 (xsd:integer)
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • Le THK-5 était un avion de transport civil construit en Turquie durant les années 1940. (fr)
  • The THK-5 was a twin-engine aircraft designed by Stanisław Rogalski and built in Turkey in 1945 as an air ambulance. It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A and three examples of an improved version of the 5A designated THK-10. A single example of the type was exported, sold to Denmark. (en)
rdfs:label
  • THK-5 (fr)
  • THK-5 (en)
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