DBpedia 2016-04

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IIL_IS-10 abstract "The IIL IS-10 was a high performance, single seat glider, designed and built in Romania in the early 1960s. It was the first Romanian aircraft to use laminar flow airfoils.".
IIL_IS-10 origin Romania.
IIL_IS-10 predecessor IIL_IS-4.
IIL_IS-10 type Glider_(sailplane).
IIL_IS-10 wikiPageID "41671916".
IIL_IS-10 wikiPageLength "6655".
IIL_IS-10 wikiPageOutDegree "39".
IIL_IS-10 wikiPageRevisionID "668399788".
IIL_IS-10 wikiPageWikiLink Aileron.
IIL_IS-10 wikiPageWikiLink Aircraft_canopy.
IIL_IS-10 wikiPageWikiLink Aircraft_fabric_covering.
IIL_IS-10 wikiPageWikiLink Airfoil.
IIL_IS-10 wikiPageWikiLink Cantilever.
IIL_IS-10 wikiPageWikiLink Category:Romanian_sailplanes_1960–1969.
IIL_IS-10 wikiPageWikiLink Chord_(aeronautics).
IIL_IS-10 wikiPageWikiLink Dihedral_(aeronautics).
IIL_IS-10 wikiPageWikiLink Elevator_(aeronautics).
IIL_IS-10 wikiPageWikiLink Empennage.
IIL_IS-10 wikiPageWikiLink Fin.
IIL_IS-10 wikiPageWikiLink Fuselage.
IIL_IS-10 wikiPageWikiLink Fédération_Aéronautique_Internationale.
IIL_IS-10 wikiPageWikiLink Glider_(sailplane).
IIL_IS-10 wikiPageWikiLink Glider_competition_classes.
IIL_IS-10 wikiPageWikiLink IIL_IS-4.
IIL_IS-10 wikiPageWikiLink Laminar_flow.
IIL_IS-10 wikiPageWikiLink Landing_gear.
IIL_IS-10 wikiPageWikiLink Leading_edge.
IIL_IS-10 wikiPageWikiLink Monocoque.
IIL_IS-10 wikiPageWikiLink Monoplane.
IIL_IS-10 wikiPageWikiLink NACA_airfoil.
IIL_IS-10 wikiPageWikiLink Plywood.
IIL_IS-10 wikiPageWikiLink Poly(methyl_methacrylate).
IIL_IS-10 wikiPageWikiLink Romania.
IIL_IS-10 wikiPageWikiLink Rudder.
IIL_IS-10 wikiPageWikiLink Spar_(aeronautics).
IIL_IS-10 wikiPageWikiLink Spoiler_(aeronautics).
IIL_IS-10 wikiPageWikiLink Tailplane.
IIL_IS-10 wikiPageWikiLink Trailing_edge.
IIL_IS-10 wikiPageWikiLink Wing_tip.
IIL_IS-10 wikiPageWikiLinkText "ICA IS-10".
IIL_IS-10 wikiPageWikiLinkText "IIL IS-10".
IIL_IS-10 airfoil "NACA 634621 root, 632618 from mid span outwards".
IIL_IS-10 aspectRatio "17".
IIL_IS-10 crew "One".
IIL_IS-10 designer "Iosif Silimon".
IIL_IS-10 developedFrom IIL_IS-4.
IIL_IS-10 emptyWeightKg "240".
IIL_IS-10 firstFlight "1960-04-06".
IIL_IS-10 glideRatio "best 32.7 at".
IIL_IS-10 grossWeightKg "340".
IIL_IS-10 heightM "1.6".
IIL_IS-10 lengthM "7.44".
IIL_IS-10 manufacturer "Intreprinderea de industrie Locală".
IIL_IS-10 nationalOrigin Romania.
IIL_IS-10 neverExceedSpeedKmh "230".
IIL_IS-10 neverExceedSpeedNote "placard, in smooth air *Rough air speed max: *Aerotow speed: *Winch launch speed:".
IIL_IS-10 primeUnits%3F_ "met".
IIL_IS-10 ref "Sailplanes of the World, pp.202-3".
IIL_IS-10 sinkRateMs "0.67".
IIL_IS-10 sinkRateNote "minimum, at".
IIL_IS-10 spanM "15".
IIL_IS-10 stallSpeedKmh "62".
IIL_IS-10 type "Single seat glider".
IIL_IS-10 wikiPageUsesTemplate Template:Aircontent.
IIL_IS-10 wikiPageUsesTemplate Template:Aircraft_specs.
IIL_IS-10 wikiPageUsesTemplate Template:Convert.
IIL_IS-10 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
IIL_IS-10 wikiPageUsesTemplate Template:Iosif_Silimon_aircraft.
IIL_IS-10 wikiPageUsesTemplate Template:Reflist.
IIL_IS-10 wingAreaSqm "13.2".
IIL_IS-10 m "25.7".
IIL_IS-10 subject Category:Romanian_sailplanes_1960–1969.
IIL_IS-10 hypernym Performance.
IIL_IS-10 type Aircraft.
IIL_IS-10 type Album.
IIL_IS-10 type MeanOfTransportation.
IIL_IS-10 type Product.
IIL_IS-10 type DesignedArtifact.
IIL_IS-10 type Thing.
IIL_IS-10 type Q11436.
IIL_IS-10 comment "The IIL IS-10 was a high performance, single seat glider, designed and built in Romania in the early 1960s. It was the first Romanian aircraft to use laminar flow airfoils.".
IIL_IS-10 label "IIL IS-10".
IIL_IS-10 sameAs Q17079953.
IIL_IS-10 sameAs m.0_ft1nq.
IIL_IS-10 sameAs Q17079953.
IIL_IS-10 wasDerivedFrom IIL_IS-10?oldid=668399788.
IIL_IS-10 isPrimaryTopicOf IIL_IS-10.