About: IIL IS-9

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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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http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FIIL_IS-9&invfp=IFP_OFF&sas=SAME_AS_OFF

The IIL IS-9 was a low powered, experimental pod and boom style motor glider, designed and built in Romania in the late 1950s.

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	IIL IS-9 (en)
rdfs:comment	The IIL IS-9 was a low powered, experimental pod and boom style motor glider, designed and built in Romania in the late 1950s. (en)
dcterms:subject	Motor gliders 1950s Romanian civil aircraft
Wikipage page ID	41662187 (xsd:integer)
Wikipage revision ID	997578562 (xsd:integer)
Link from a Wikipage to another Wikipage	Propeller (aircraft) Romania NACA airfoil Perspex Elevator (aircraft) Wing tip Empennage Plywood Trim tab Aileron Fuselage Leading edge Aircraft fabric covering Fin Balanced rudder Monocoque Trailing edge Motor glider Motor gliders 1950s Romanian civil aircraft Tailplane IIL IS-5 IIL IS-7 IIL IS-8 Air brake (aircraft) Canopy (aircraft) Experimental aircraft Dihedral (aircraft) Spar (aviation) High wing Tricycle gear dbr:IIL_(aircraft_manufacturer)
sameAs	IIL IS-9 IIL IS-9 IIL IS-9
sink rate ms	0.850000 (xsd:double)
sink rate note	minimum, at . Jane's 1962 data give slightly poorer best glide ratio and sink rate, at lower speeds (en)
span m	12 (xsd:integer)
stall speed kmh	52 (xsd:integer)
wing area sqm	15 (xsd:integer)
wing loading kg/m	24 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type dbt:Iosif_Silimon_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1958-07-02 (xsd:date)
national origin	Romania
crew	One (en)
designer	Iosif Silimon (en)
manufacturer	Intreprinderea de industrie Locală (en)
ref	Sailplanes of the World, pp.200-1 (en)
type	Single seat motor glider (en)
has abstract	The IIL IS-9 was a low powered, experimental pod and boom style motor glider, designed and built in Romania in the late 1950s. (en)
airfoil	NACA 43015 root, 43012A from mid span outwards (en)
aspect ratio	11.300000 (xsd:double)
developed from	IIL IS-5
empty weight kg	230 (xsd:integer)
eng1 hp	20 (xsd:integer)
eng1 name	unknown (en)
eng1 number	1 (xsd:integer)
glide ratio	best 23.5 at (en)
gross weight kg	360 (xsd:integer)
height m	2.740000 (xsd:double)
length m	6.640000 (xsd:double)
never exceed speed kmh	180 (xsd:integer)
never exceed speed note	placard, in smooth air Rough air speed max: Aerotow speed: (en)
number built	1 (xsd:integer)
prop blade number	2 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:IIL_IS-9?oldid=997578562&ns=0
page length (characters) of wiki page	7267 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
origin	Romania
predecessor	IIL IS-5
type	Motor glider
foaf:isPrimaryTopicOf	wikipedia-en:IIL_IS-9
is Link from a Wikipage to another Wikipage of	List of gliders (I)
is foaf:primaryTopic of	wikipedia-en:IIL_IS-9

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