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The PIK-5 was a training glider produced in Finland in the 1940s, and 1950s, equipping the country's gliding clubs with an aircraft greater in performance than primary gliders but less than competition sailplanes. The PIK-5 had a pod-and-boom configuration, with a high, strut-braced monoplane wing and a cruciform tail carried at the end of a tail boom that extended from a position high on the aft end of the pod.

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rdf:type
rdfs:label
  • PIK-5 (en)
rdfs:comment
  • The PIK-5 was a training glider produced in Finland in the 1940s, and 1950s, equipping the country's gliding clubs with an aircraft greater in performance than primary gliders but less than competition sailplanes. The PIK-5 had a pod-and-boom configuration, with a high, strut-braced monoplane wing and a cruciform tail carried at the end of a tail boom that extended from a position high on the aft end of the pod. (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/PIK-5b.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
sink rate ms
sink rate note
  • at (en)
span m
stall speed kmh
wing area sqm
wing loading kg/m
dbp:wikiPageUsesTemplate
thumbnail
dbp:primeUnits%3F_
  • met (en)
first flight
  • September 1946 (en)
national origin
  • Finland (en)
crew
designer
  • Kaarlo J. Temmes (en)
manufacturer
ref
  • Karhulan Ilmailukerho website : PIK-5c Cumulus , The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (en)
type
  • Training glider (en)
has abstract
  • The PIK-5 was a training glider produced in Finland in the 1940s, and 1950s, equipping the country's gliding clubs with an aircraft greater in performance than primary gliders but less than competition sailplanes. The PIK-5 had a pod-and-boom configuration, with a high, strut-braced monoplane wing and a cruciform tail carried at the end of a tail boom that extended from a position high on the aft end of the pod. (en)
airfoil
  • Göttingen 533 (en)
aspect ratio
empty weight kg
g limits
  • +4 -2 (en)
glide ratio
length m
max takeoff weight kg
never exceed speed kmh
never exceed speed note
  • *Rough air speed max: *Aerotow speed: *Winch launch speed: *Terminal velocity: with full air-brakes at max all-up weight (en)
number built
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page length (characters) of wiki page
number built
manufacturer
origin
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