About: Collins X-112

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org:8891 associated with source document(s)
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http://dbpedia.org:8891/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FCollins_X-112

The Collins X-112 was an experimental two-seat ground-effect vehicle, designed by Alexander Lippisch in the United States in the early 1960s to test his thick reverse delta wing concept.

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	Collins X-112 (en) X-112 (fr)
rdfs:comment	The Collins X-112 was an experimental two-seat ground-effect vehicle, designed by Alexander Lippisch in the United States in the early 1960s to test his thick reverse delta wing concept. (en) Le X-112 airfoil boat est un hydravion à effet de sol expérimental, destiné à expérimenter un nouveau type de transport maritime rapide. C'est le premier WIG (Wing In Ground effect) de l'ingénieur allemand Alexander Lippisch, travaillant pour le compte de la société Collins aux États-Unis. Précédé par de nombreux essais sur des modèles à l'échelle 1/8 et 1/4 testés en bassin de carène et en soufflerie, ce prototype a été dessiné et construit en 1961-62 et testé en 1963. Ce prototype est exposé au EAA Museum à Oshkosh (États-Unis). EAA : Experimental Aircraft Association (fr)
dcterms:subject	Ground effect vehicles Low-wing aircraft Single-engined tractor aircraft T-tail aircraft 1960s United States experimental aircraft Aircraft first flown in 1963
Wikipage page ID	40672090 (xsd:integer)
Wikipage revision ID	1121851257 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane Elevator (aircraft) Wing tip Ekranoplan Ground effect vehicles Delta wing Tandem Low-wing aircraft Cedar Rapids, Iowa Aileron Fuselage Leading edge Airfoil Alexander Lippisch Single-engined tractor aircraft T-tail aircraft Fibreglass Fin Flight dynamics (fixed-wing aircraft) Collins Radio Company Trailing edge Ground effect vehicle Ground-effect vehicle 1960s United States experimental aircraft Tractor configuration Aircraft first flown in 1963 Aspect ratio (wing) RFB X-113 Rudder Wing root Dihedral (aircraft) Air cushion vehicle Winglet
Link from a Wikipage to an external page	http://seaplanemagazine.com/2018/03/22/x-112-aerofoil-boat-great-old-footage/ https://web.archive.org/web/20180326230840/http:/seaplanemagazine.com/2018/03/22/x-112-aerofoil-boat-great-old-footage/ https://www.youtube.com/watch%3Fv=wlIK-xViG_4
sameAs	Collins X-112 Collins X-112 Collins X-112 Collins X-112
span ft	14 (xsd:integer)
span in	0 (xsd:integer)
wing area sqft	110 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Lippisch_aircraft dbt:As_of dbt:Cite_magazine dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	imp (en)
first flight	1963 (xsd:integer)
national origin	United States (en)
crew	One or two (en)
designer	Alexander Lippisch
length ft	25 (xsd:integer)
manufacturer	Collins Radio Company (en)
ref	Jane's All the World's Aircraft (en)
type	Ground effect vehicle
has abstract	The Collins X-112 was an experimental two-seat ground-effect vehicle, designed by Alexander Lippisch in the United States in the early 1960s to test his thick reverse delta wing concept. (en) Le X-112 airfoil boat est un hydravion à effet de sol expérimental, destiné à expérimenter un nouveau type de transport maritime rapide. C'est le premier WIG (Wing In Ground effect) de l'ingénieur allemand Alexander Lippisch, travaillant pour le compte de la société Collins aux États-Unis. Précédé par de nombreux essais sur des modèles à l'échelle 1/8 et 1/4 testés en bassin de carène et en soufflerie, ce prototype a été dessiné et construit en 1961-62 et testé en 1963. Ce prototype est exposé au EAA Museum à Oshkosh (États-Unis). EAA : Experimental Aircraft Association (fr)
developed into	RFB X-113
empty weight lb	370 (xsd:integer)
eng1 hp	25 (xsd:integer)
eng1 name	unknown, tractor configuration (en)
eng1 number	1 (xsd:integer)
gross weight lb	710 (xsd:integer)
length in	0 (xsd:integer)
max speed mph	77 (xsd:integer)
max speed note	in free flight, flown solo (en)
more performance	* Take-off speed: 35—38 mph (en)
number built	1 (xsd:integer)
prop name	fixed pitch (en)

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