About: Horikawa H-22

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The Horikawa H-22B-3 is a simple, open frame, two seat primary trainer glider designed and built in Japan in the 1950s.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Horikawa H-22 (en)
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)
dcterms:subject	1950s Japanese aircraft
Wikipage page ID	36705271 (xsd:integer)
Wikipage revision ID	936159525 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Elevator (aircraft) Tandem Fuselage Aircraft fabric covering Fin Glider (sailplane) Trailing edge Japan Chord (aircraft) Landing gear 1950s Japanese aircraft Tailplane Spoiler (aeronautics) World War II Rudder Dihedral (aircraft) Trainer aircraft Stamer Lippisch Zögling
Link from a Wikipage to an external page
sameAs	Horikawa H-22 Horikawa H-22
sink rate ms	1.160000 (xsd:double)
sink rate note	minimum at 54.4 km/h; 29.3 kn (en)
span m	12.210000 (xsd:double)
stall speed kmh	48.500000 (xsd:double)
wing area sqm	16.800000 (xsd:double)
wing loading kg/m	17.800000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	August 1953 (en)
national origin	Japan
crew	Two (en)
designer	Ikuo Horikawa (en)
manufacturer	Hagiwara Kakkuki Seisakusho (en)
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)
type	Two seat Primary trainer glider (en)
has 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)
airfoil	Göttingen 532 (en)
aspect ratio	8.870000 (xsd:double)
empty weight kg	170 (xsd:integer)
empty weight note	equipped (en)
glide ratio	14.200000 (xsd:double)
gross weight kg	300 (xsd:integer)
length m	7 (xsd:integer)
never exceed speed kmh	120 (xsd:integer)
never exceed speed note	in smooth air (en) Rough air speed max: Winch launch speed: (en)
number built	at least 30 (en)
prov:wasDerivedFrom	wikipedia-en:Horikawa_H-22?oldid=936159525&ns=0
page length (characters) of wiki page	6463 (xsd:nonNegativeInteger)
origin	Japan
type	Trainer aircraft
foaf:isPrimaryTopicOf	wikipedia-en:Horikawa_H-22
is Link from a Wikipage to another Wikipage of	List of gliders (H) Horikawa H-22B-3 H22 Hagiwara H-22 Hagiwara H-22B-3
is Wikipage redirect of	Horikawa H-22B-3 Hagiwara H-22 Hagiwara H-22B-3
is foaf:primaryTopic of	wikipedia-en:Horikawa_H-22

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