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- IIL_IS-12 abstract "The IIL IS-12 was a two seat glider, designed and built in Romania in 1960. It had a wooden wing but a metal fuselage and was constructed in parallel with the all-wood IS-13 for comparative tests. It was later followed by the IS-13a, a version with an all-metal wing.".
- IIL_IS-12 numberBuilt "1".
- IIL_IS-12 origin Romania.
- IIL_IS-12 type Trainer_(aircraft).
- IIL_IS-12 wikiPageID "41685612".
- IIL_IS-12 wikiPageLength "8318".
- IIL_IS-12 wikiPageOutDegree "32".
- IIL_IS-12 wikiPageRevisionID "668399797".
- IIL_IS-12 wikiPageWikiLink Aileron.
- IIL_IS-12 wikiPageWikiLink Aircraft_canopy.
- IIL_IS-12 wikiPageWikiLink Aircraft_fabric_covering.
- IIL_IS-12 wikiPageWikiLink Aircraft_fairing.
- IIL_IS-12 wikiPageWikiLink Balanced_rudder.
- IIL_IS-12 wikiPageWikiLink Cantilever.
- IIL_IS-12 wikiPageWikiLink Category:Romanian_sailplanes_1960–1969.
- IIL_IS-12 wikiPageWikiLink Chord_(aeronautics).
- IIL_IS-12 wikiPageWikiLink Elevator_(aeronautics).
- IIL_IS-12 wikiPageWikiLink Empennage.
- IIL_IS-12 wikiPageWikiLink Fin.
- IIL_IS-12 wikiPageWikiLink Fuselage.
- IIL_IS-12 wikiPageWikiLink Glider_(sailplane).
- IIL_IS-12 wikiPageWikiLink Landing_gear.
- IIL_IS-12 wikiPageWikiLink Leading_edge.
- IIL_IS-12 wikiPageWikiLink Monocoque.
- IIL_IS-12 wikiPageWikiLink NACA_airfoil.
- IIL_IS-12 wikiPageWikiLink Plywood.
- IIL_IS-12 wikiPageWikiLink Poly(methyl_methacrylate).
- IIL_IS-12 wikiPageWikiLink Romania.
- IIL_IS-12 wikiPageWikiLink Spar_(aeronautics).
- IIL_IS-12 wikiPageWikiLink Spoiler_(aeronautics).
- IIL_IS-12 wikiPageWikiLink Tandem.
- IIL_IS-12 wikiPageWikiLink Trailing_edge.
- IIL_IS-12 wikiPageWikiLink Trainer_(aircraft).
- IIL_IS-12 wikiPageWikiLink Trim_tab.
- IIL_IS-12 wikiPageWikiLink Wing_tip.
- IIL_IS-12 wikiPageWikiLinkText "ICA IS-12".
- IIL_IS-12 wikiPageWikiLinkText "ICA IS-13".
- IIL_IS-12 wikiPageWikiLinkText "IIL IS-12".
- IIL_IS-12 airfoil "NACA 43015 root, 43012A tip".
- IIL_IS-12 aspectRatio "12.5".
- IIL_IS-12 crew "Two".
- IIL_IS-12 designer "Iosif Silimon".
- IIL_IS-12 emptyWeightKg "290".
- IIL_IS-12 firstFlight "1960-12-23".
- IIL_IS-12 gLimits "+5/-3".
- IIL_IS-12 glideRatio "best 24 at".
- IIL_IS-12 grossWeightKg "480".
- IIL_IS-12 lengthM "7.6".
- IIL_IS-12 manufacturer "Întreprinderea de industrie Locală".
- IIL_IS-12 nationalOrigin Romania.
- IIL_IS-12 neverExceedSpeedKmh "200".
- IIL_IS-12 neverExceedSpeedNote "placard, in smooth air *Rough air speed max: *Aerotow speed: *Winch launch speed:".
- IIL_IS-12 numberBuilt "1".
- IIL_IS-12 primeUnits%3F_ "met".
- IIL_IS-12 ref "Sailplanes of the World, pp.206-7".
- IIL_IS-12 sinkRateMs "0.92".
- IIL_IS-12 sinkRateNote "minimum, at".
- IIL_IS-12 spanM "15".
- IIL_IS-12 stallSpeedKmh "58".
- IIL_IS-12 type "Experimental two seat trainer glider".
- IIL_IS-12 wikiPageUsesTemplate Template:Aircontent.
- IIL_IS-12 wikiPageUsesTemplate Template:Aircraft_specs.
- IIL_IS-12 wikiPageUsesTemplate Template:Convert.
- IIL_IS-12 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- IIL_IS-12 wikiPageUsesTemplate Template:Iosif_Silimon_aircraft.
- IIL_IS-12 wikiPageUsesTemplate Template:Reflist.
- IIL_IS-12 wingAreaSqm "18".
- IIL_IS-12 m "26.6".
- IIL_IS-12 subject Category:Romanian_sailplanes_1960–1969.
- IIL_IS-12 hypernym Glider.
- IIL_IS-12 type Aircraft.
- IIL_IS-12 type MeanOfTransportation.
- IIL_IS-12 type Product.
- IIL_IS-12 type DesignedArtifact.
- IIL_IS-12 type Thing.
- IIL_IS-12 type Q11436.
- IIL_IS-12 comment "The IIL IS-12 was a two seat glider, designed and built in Romania in 1960. It had a wooden wing but a metal fuselage and was constructed in parallel with the all-wood IS-13 for comparative tests. It was later followed by the IS-13a, a version with an all-metal wing.".
- IIL_IS-12 label "IIL IS-12".
- IIL_IS-12 sameAs Q17079982.
- IIL_IS-12 sameAs m.0_fs6yj.
- IIL_IS-12 sameAs Q17079982.
- IIL_IS-12 wasDerivedFrom IIL_IS-12?oldid=668399797.
- IIL_IS-12 isPrimaryTopicOf IIL_IS-12.