dbo:abstract |
The Horikawa H-22B-3 is a simple, open frame, two seat primary trainer glider designed and built in Japan in the 1950s. (en) |
dbo:origin |
dbr:Japan |
dbo:type |
dbr:Trainer_aircraft |
dbo:wikiPageExternalLink |
https://web.archive.org/web/20120908060339/http:/www.ae.illinois.edu/m-selig/ads/afplots/goe532.gif |
dbo:wikiPageID |
36705271 (xsd:integer) |
dbo:wikiPageLength |
6463 (xsd:nonNegativeInteger) |
dbo:wikiPageRevisionID |
936159525 (xsd:integer) |
dbo:wikiPageWikiLink |
dbr:Monoplane dbr:Elevator_(aircraft) dbr:Tandem dbr:Fuselage dbr:Aircraft_fabric_covering dbr:Fin dbr:Glider_(sailplane) dbr:Trailing_edge dbr:Japan dbr:Chord_(aircraft) dbr:Landing_gear dbc:1950s_Japanese_aircraft dbr:Tailplane dbr:Spoiler_(aeronautics) dbr:World_War_II dbr:Rudder dbr:Dihedral_(aircraft) dbr:Trainer_aircraft dbr:Stamer_Lippisch_Zögling |
dbp:airfoil |
Göttingen 532 (en) |
dbp:aspectRatio |
8.870000 (xsd:double) |
dbp:crew |
Two (en) |
dbp:designer |
Ikuo Horikawa (en) |
dbp:emptyWeightKg |
170 (xsd:integer) |
dbp:emptyWeightNote |
equipped (en) |
dbp:firstFlight |
August 1953 (en) |
dbp:glideRatio |
14.200000 (xsd:double) |
dbp:grossWeightKg |
300 (xsd:integer) |
dbp:lengthM |
7 (xsd:integer) |
dbp:manufacturer |
Hagiwara Kakkuki Seisakusho (en) |
dbp:nationalOrigin |
dbr:Japan |
dbp:neverExceedSpeedKmh |
120 (xsd:integer) |
dbp:neverExceedSpeedNote |
in smooth air (en) *Rough air speed max: *Winch launch speed: (en) |
dbp:numberBuilt |
at least 30 (en) |
dbp:primeUnits?_ |
met (en) |
dbp:ref |
Jane's All the World's Aircraft 1966-67 The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (en) |
dbp:sinkRateMs |
1.160000 (xsd:double) |
dbp:sinkRateNote |
minimum at 54.4 km/h; 29.3 kn (en) |
dbp:spanM |
12.210000 (xsd:double) |
dbp:stallSpeedKmh |
48.500000 (xsd:double) |
dbp:type |
Two seat Primary trainer glider (en) |
dbp:wikiPageUsesTemplate |
dbt:Convert dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type |
dbp:wingAreaSqm |
16.800000 (xsd:double) |
dbp:wingLoadingKg/m |
17.800000 (xsd:double) |
dcterms:subject |
dbc:1950s_Japanese_aircraft |
rdf:type |
owl:Thing schema:Product dbo:MeanOfTransportation wikidata:Q11436 dbo:Aircraft |
rdfs:comment |
The Horikawa H-22B-3 is a simple, open frame, two seat primary trainer glider designed and built in Japan in the 1950s. (en) |
rdfs:label |
Horikawa H-22 (en) |
owl:sameAs |
wikidata:Horikawa H-22 https://global.dbpedia.org/id/fddp |
prov:wasDerivedFrom |
wikipedia-en:Horikawa_H-22?oldid=936159525&ns=0 |
foaf:isPrimaryTopicOf |
wikipedia-en:Horikawa_H-22 |
is dbo:wikiPageRedirects of |
dbr:Horikawa_H-22B-3 dbr:Hagiwara_H-22 dbr:Hagiwara_H-22B-3 |
is dbo:wikiPageWikiLink of |
dbr:List_of_gliders_(H) dbr:Horikawa_H-22B-3 dbr:H22 dbr:Hagiwara_H-22 dbr:Hagiwara_H-22B-3 |
is foaf:primaryTopic of |
wikipedia-en:Horikawa_H-22 |