About: L.A.D. Mita 3

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The Kirigamine Mita is a training glider, seating two in tandem, designed in Japan in the early 1960s. A modified version, first flown in 1966, was produced in modest numbers.

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
rdfs:label	L.A.D. Mita 3 (en)
rdfs:comment	The Kirigamine Mita is a training glider, seating two in tandem, designed in Japan in the early 1960s. A modified version, first flown in 1966, was produced in modest numbers. (en)
dcterms:subject	Shoulder-wing aircraft Aircraft first flown in 1962 1960s Japanese aircraft
Wikipage page ID	36705274 (xsd:integer)
Wikipage revision ID	1119548368 (xsd:integer)
Link from a Wikipage to another Wikipage	NACA airfoil Elevator (aircraft) Shoulder wing Plywood Tandem Aileron Fuselage Leading edge Aircraft fabric covering Fin Glider (sailplane) Dorsal (anatomy) Japan Shoulder-wing aircraft Aircraft first flown in 1962 Chord (aircraft) Kakamigahara Laminar flow Landing gear Cockpit 1960s Japanese aircraft Fillet (mechanics) Fairing (aircraft) Air brake (aircraft) Canopy (aircraft) Rudder Schempp-Hirth Trainer aircraft Glass reinforced plastic Wing tips
Link from a Wikipage to an external page
sameAs	L.A.D. Mita 3 L.A.D. Mita 3 L.A.D. Mita 3
sink rate ftmin	142 (xsd:integer)
sink rate note	minimum at 76 km/h (en)
span m	16 (xsd:integer)
wing area sqm	15.870000 (xsd:double)
wing loading kg/m	28.400000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	1962 (xsd:integer)
national origin	Japan
crew	Two (en)
designer	Asahi Miyahara (en)
height ft	4 (xsd:integer)
height in	2.500000 (xsd:double)
manufacturer	Kirigamine Glider Manufacturing Co/ Light Aircraft Development Co. / Tainan Industry Co. (en)
ref	Sailplanes 1965-2000; Gliders and Sailplanes of the World (en)
type	Two seat trainer glider (en)
has abstract	The Kirigamine Mita is a training glider, seating two in tandem, designed in Japan in the early 1960s. A modified version, first flown in 1966, was produced in modest numbers. (en)
airfoil	NACA 633618 (en)
aspect ratio	16.130000 (xsd:double)
empty weight kg	300 (xsd:integer)
glide ratio	30 (xsd:integer)
gross weight kg	450 (xsd:integer)
length m	7.770000 (xsd:double)
max speed mph	118 (xsd:integer)
max speed note	in smooth air (en)
number built	37 (xsd:integer)
perfhide	Y (en)
gold:hypernym	Glider
prov:wasDerivedFrom	wikipedia-en:L.A.D._Mita_3?oldid=1119548368&ns=0
page length (characters) of wiki page	6972 (xsd:nonNegativeInteger)
number built	37 (xsd:nonNegativeInteger)
origin	Japan
type	Trainer aircraft
foaf:isPrimaryTopicOf	wikipedia-en:L.A.D._Mita_3
is Link from a Wikipage to another Wikipage of	L.A.D. Mita 3 Kai 1 Tainan Mita 3 Tainan Mita III Kirigamine Mita 3
is Wikipage redirect of	L.A.D. Mita 3 Kai 1 Tainan Mita 3 Tainan Mita III Kirigamine Mita 3

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