About: IIL IS-5

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The IIL IS-5 was a single seat, high performance sailplane designed by Iosif Șilimon and built in Romania in 1960.

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 settlement yago:Type105840188
rdfs:label	IIL IS-5 (en)
rdfs:comment	The IIL IS-5 was a single seat, high performance sailplane designed by Iosif Șilimon and built in Romania in 1960. (en)
differentFrom	IS-5 Kaczka
dcterms:subject	1960s Romanian sailplanes
Wikipage page ID	41637967 (xsd:integer)
Wikipage revision ID	993147829 (xsd:integer)
Link from a Wikipage to another Wikipage	Romania NACA airfoil Monoplane Perspex Elevator (aircraft) Sailplane Shoulder wing Empennage Plywood Aileron URMV-3 IS-3 Fuselage Leading edge Aircraft canopy Aircraft fabric covering Aircraft fairing Fin Balanced rudder Monocoque Trailing edge Iosif Șilimon Landing gear Cockpit 1960s Romanian sailplanes Tailplane Air brake (aircraft) Cantilever Dihedral (aircraft) Spar (aviation)
Link from a Wikipage to an external page
sameAs	IIL IS-5 IIL IS-5 IIL IS-5
sink rate ms	0.740000 (xsd:double)
sink rate note	minimum, at (en)
span m	15 (xsd:integer)
stall speed kmh	55 (xsd:integer)
wing area sqm	15 (xsd:integer)
wing loading kg/m	20.900000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Distinguish dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type dbt:Iosif_Silimon_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1960-06-14 (xsd:date)
national origin	Romania
crew	One (en)
designer	Iosif Șilimon
manufacturer	Intreprinderea de industrie Locală (en)
ref	The World's Sailplanes , pp.194-5 (en)
type	Single seat high performance Sailplane (en)
has abstract	The IIL IS-5 was a single seat, high performance sailplane designed by Iosif Șilimon and built in Romania in 1960. (en)
airfoil	NACA airfoil
aspect ratio	15 (xsd:integer)
developed from	URMV-3 IS-3
empty weight kg	220 (xsd:integer)
empty weight note	equipped (en)
glide ratio	best, 28:1 at (en)
gross weight kg	320 (xsd:integer)
length m	6.360000 (xsd:double)
never exceed speed kmh	180 (xsd:integer)
never exceed speed note	placard, smooth air Rough air speed max: Aerotow speed: *Winch launch speed: (en)
gold:hypernym	Seat
prov:wasDerivedFrom	wikipedia-en:IIL_IS-5?oldid=993147829&ns=0
page length (characters) of wiki page	5508 (xsd:nonNegativeInteger)
designer	Iosif Șilimon
origin	Romania
predecessor	URMV-3 IS-3
type	Sailplane
foaf:isPrimaryTopicOf	wikipedia-en:IIL_IS-5
is Link from a Wikipage to another Wikipage of	List of aircraft (I) List of gliders (I) List of Romanian gliders Iosif Șilimon IIL IS-8

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