About: Kimura HK-1

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The Kimura HK-1 was a glider built in Japan in 1939 to investigate the possibilities of tailless aircraft. It was a single-seat design with an open cockpit, swept wings, and a single tail fin. The HK-1 made a total of 169 test flights between 15 December 1939 and 7 March 1940, towed aloft behind a car.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188 umbel-rc:Model_airplane
rdfs:label	Kimura HK-1 (en) かつをどり (航空機) (ja) Kimura HK-1 (pt)
rdfs:comment	かつをどり（かつおどり）は、萱場製作所（現KYB）が大日本帝国陸軍向けに計画したラムジェットエンジン搭載の無尾翼近距離戦闘機。本頁ではかつをどり実現に向けて製作された試作機についても記述する。無動力の試作機が事故を起こしたために計画は中止され、かつをどりの実機は製造されることなく終わった。 (ja) The Kimura HK-1 was a glider built in Japan in 1939 to investigate the possibilities of tailless aircraft. It was a single-seat design with an open cockpit, swept wings, and a single tail fin. The HK-1 made a total of 169 test flights between 15 December 1939 and 7 March 1940, towed aloft behind a car. (en) O Kimura HK-1 foi um planador construído no Japão em 1939, cuja missão era a de investigar a possibilidade de construção de aeronaves sem cauda. Este planador tinha um único lugar com um cockpit aberto e asas em flecha. O HK-1 realizou 169 voos de teste entre 15 de Dezembro de 1939 e 7 de Março de 1940, sempre preso por uma corda atrás de um carro. (pt)
foaf:depiction
dcterms:subject	Kayaba aircraft 1930s Japanese experimental aircraft Aircraft first flown in 1939 Glider aircraft Tailless aircraft
Wikipage page ID	18495206 (xsd:integer)
Wikipage revision ID	1121226634 (xsd:integer)
Link from a Wikipage to another Wikipage	Kayaba aircraft 1930s Japanese experimental aircraft Kayaba Ku-2 Aircraft first flown in 1939 Glider aircraft Tailless aircraft Tachikawa Aircraft Company Ltd Imperial Japanese Army Tailless aircraft dbr:Hidemasa_Kimura
Link from a Wikipage to an external page	http://www.defence.org.cn/article-10-15944.html http://www.century-of-flight.net/Aviation%20history/flying%20wings/japan.htm
sameAs	Kimura HK-1 Kimura HK-1 Kimura HK-1 Kimura HK-1 Kimura HK-1
span ft	32 (xsd:integer)
span in	10 (xsd:integer)
span m	10 (xsd:integer)
wing area sqft	151 (xsd:integer)
wing area sqm	14 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Kayaba_aircraft dbt:Cite_web dbt:Commons_category dbt:More_citations_needed dbt:Multiple_issues dbt:No_footnotes dbt:Short_description dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/KN_Kayaba_HK1_1939.jpg?width=300
dbp:primeUnits%3F_	met (en)
national origin	Japan (en)
crew	One pilot (en)
designer	dbr:Hidemasa_Kimura
height ft	5 (xsd:integer)
height in	11 (xsd:integer)
introduced	1939 (xsd:integer)
length ft	11 (xsd:integer)
manufacturer	Ito Airplane Works (en)
retired	1940 (xsd:integer)
status	Cancelled (en)
type	Research glider (en)
has abstract	The Kimura HK-1 was a glider built in Japan in 1939 to investigate the possibilities of tailless aircraft. It was a single-seat design with an open cockpit, swept wings, and a single tail fin. The HK-1 made a total of 169 test flights between 15 December 1939 and 7 March 1940, towed aloft behind a car. By this time, the glider's success had attracted the attention of the Army, which arranged to purchase the aircraft. It was taken to the Tachikawa factory for testing, but was crashed after only 13 flights, on 16 April 1940. The design proved sufficiently interesting for the Army to commission further research into the tailless concept, which would lead to the Kayaba Ku-2. (en) かつをどり（かつおどり）は、萱場製作所（現KYB）が大日本帝国陸軍向けに計画したラムジェットエンジン搭載の無尾翼近距離戦闘機。本頁ではかつをどり実現に向けて製作された試作機についても記述する。無動力の試作機が事故を起こしたために計画は中止され、かつをどりの実機は製造されることなく終わった。 (ja) O Kimura HK-1 foi um planador construído no Japão em 1939, cuja missão era a de investigar a possibilidade de construção de aeronaves sem cauda. Este planador tinha um único lugar com um cockpit aberto e asas em flecha. O HK-1 realizou 169 voos de teste entre 15 de Dezembro de 1939 e 7 de Março de 1940, sempre preso por uma corda atrás de um carro. Por esta altura, o sucesso do planador atraiu a atenção do Exército Imperial Japonês, que fez os possíveis para comprar o planador. Assim, o HK-1 foi levado para uma fábrica em Tachikawa e foi testado; depois de alguns voos, o planador despenhou-se no dia 16 de Abril de 1940. O design provou ser interessante e promissor o suficiente para o Exército o submeter a mais pesquisas e testes, o que levaria ao desenvolvimento do . (pt)
developed into	Kayaba Ku-2
height m	1.800000 (xsd:double)
length in	6 (xsd:integer)
length m	3.500000 (xsd:double)
max speed kmh	85 (xsd:integer)
max speed mph	53 (xsd:integer)
number built	1 (xsd:integer)
gold:hypernym	Glider
prov:wasDerivedFrom	wikipedia-en:Kimura_HK-1?oldid=1121226634&ns=0
page length (characters) of wiki page	2810 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
designer	dbr:Hidemasa_Kimura
foaf:isPrimaryTopicOf	wikipedia-en:Kimura_HK-1
is Link from a Wikipage to another Wikipage of	List of aircraft (K) List of experimental aircraft List of accidents and incidents involving military aircraft (1940–1942) List of gliders (K) Kayaba Ku-2 List of Japanese gliders KYB Corporation HK1 (disambiguation) Kumazō Hino

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