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- IIL_IS-5 abstract "The IIL IS-5 was a single seat, high performance sailplane designed by Iosif Silimons and built in Romania in 1960.".
- IIL_IS-5 origin Romania.
- IIL_IS-5 predecessor URMV-3_IS-3.
- IIL_IS-5 type Glider_(sailplane).
- IIL_IS-5 wikiPageExternalLink naca23012.gif.
- IIL_IS-5 wikiPageExternalLink naca23015.gif.
- IIL_IS-5 wikiPageID "41637967".
- IIL_IS-5 wikiPageLength "5553".
- IIL_IS-5 wikiPageOutDegree "31".
- IIL_IS-5 wikiPageRevisionID "668399834".
- IIL_IS-5 wikiPageWikiLink Aileron.
- IIL_IS-5 wikiPageWikiLink Air_brake_(aeronautics).
- IIL_IS-5 wikiPageWikiLink Air_brake_(aircraft).
- IIL_IS-5 wikiPageWikiLink Aircraft_canopy.
- IIL_IS-5 wikiPageWikiLink Aircraft_fabric_covering.
- IIL_IS-5 wikiPageWikiLink Aircraft_fairing.
- IIL_IS-5 wikiPageWikiLink Balanced_rudder.
- IIL_IS-5 wikiPageWikiLink Cantilever.
- IIL_IS-5 wikiPageWikiLink Category:Romanian_sailplanes_1960–1969.
- IIL_IS-5 wikiPageWikiLink Cockpit.
- IIL_IS-5 wikiPageWikiLink Dihedral_(aeronautics).
- IIL_IS-5 wikiPageWikiLink Dihedral_(aircraft).
- IIL_IS-5 wikiPageWikiLink Elevator_(aeronautics).
- IIL_IS-5 wikiPageWikiLink Elevator_(aircraft).
- IIL_IS-5 wikiPageWikiLink Empennage.
- IIL_IS-5 wikiPageWikiLink Fin.
- IIL_IS-5 wikiPageWikiLink Fuselage.
- IIL_IS-5 wikiPageWikiLink Glider_(sailplane).
- IIL_IS-5 wikiPageWikiLink Landing_gear.
- IIL_IS-5 wikiPageWikiLink Leading_edge.
- IIL_IS-5 wikiPageWikiLink Monocoque.
- IIL_IS-5 wikiPageWikiLink Monoplane.
- IIL_IS-5 wikiPageWikiLink NACA_airfoil.
- IIL_IS-5 wikiPageWikiLink Perspex.
- IIL_IS-5 wikiPageWikiLink Plywood.
- IIL_IS-5 wikiPageWikiLink Poly(methyl_methacrylate).
- IIL_IS-5 wikiPageWikiLink Romania.
- IIL_IS-5 wikiPageWikiLink Sailplane.
- IIL_IS-5 wikiPageWikiLink Shoulder_wing.
- IIL_IS-5 wikiPageWikiLink Spar_(aeronautics).
- IIL_IS-5 wikiPageWikiLink Spar_(aviation).
- IIL_IS-5 wikiPageWikiLink Tailplane.
- IIL_IS-5 wikiPageWikiLink Trailing_edge.
- IIL_IS-5 wikiPageWikiLink URMV-3_IS-3.
- IIL_IS-5 wikiPageWikiLinkText "IIL IS-5".
- IIL_IS-5 wikiPageWikiLinkText "IS-5".
- IIL_IS-5 airfoil NACA_airfoil.
- IIL_IS-5 aspectRatio "15".
- IIL_IS-5 crew "One".
- IIL_IS-5 designer "Iosif Silimon".
- IIL_IS-5 developedFrom URMV-3_IS-3.
- IIL_IS-5 emptyWeightKg "220".
- IIL_IS-5 emptyWeightNote "equipped".
- IIL_IS-5 firstFlight "1960-06-14".
- IIL_IS-5 glideRatio "best, 28:1 at".
- IIL_IS-5 grossWeightKg "320".
- IIL_IS-5 hasPhotoCollection IIL_IS-5.
- IIL_IS-5 lengthM "6.36".
- IIL_IS-5 manufacturer "Intreprinderea de industrie Locală".
- IIL_IS-5 nationalOrigin Romania.
- IIL_IS-5 neverExceedSpeedKmh "180".
- IIL_IS-5 neverExceedSpeedNote "placard, smooth air *Rough air speed max: *Aerotow speed: *Winch launch speed:".
- IIL_IS-5 primeUnits%3F_ "met".
- IIL_IS-5 ref "The World's Sailplanes , pp.194-5".
- IIL_IS-5 sinkRateMs "0.74".
- IIL_IS-5 sinkRateNote "minimum, at".
- IIL_IS-5 spanM "15".
- IIL_IS-5 stallSpeedKmh "55".
- IIL_IS-5 type "Single seat high performance Sailplane".
- IIL_IS-5 wikiPageUsesTemplate Template:Aircontent.
- IIL_IS-5 wikiPageUsesTemplate Template:Aircraft_specs.
- IIL_IS-5 wikiPageUsesTemplate Template:Convert.
- IIL_IS-5 wikiPageUsesTemplate Template:Distinguish.
- IIL_IS-5 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- IIL_IS-5 wikiPageUsesTemplate Template:Iosif_Silimon_aircraft.
- IIL_IS-5 wikiPageUsesTemplate Template:Reflist.
- IIL_IS-5 wingAreaSqm "15".
- IIL_IS-5 m "20.9".
- IIL_IS-5 subject Category:Romanian_sailplanes_1960–1969.
- IIL_IS-5 hypernym Seat.
- IIL_IS-5 type Aircraft.
- IIL_IS-5 type MeanOfTransportation.
- IIL_IS-5 type Settlement.
- IIL_IS-5 type Product.
- IIL_IS-5 type DesignedArtifact.
- IIL_IS-5 type Thing.
- IIL_IS-5 type Q11436.
- IIL_IS-5 comment "The IIL IS-5 was a single seat, high performance sailplane designed by Iosif Silimons and built in Romania in 1960.".
- IIL_IS-5 label "IIL IS-5".
- IIL_IS-5 differentFrom IS-5_Kaczka.
- IIL_IS-5 sameAs m.0_83c9r.
- IIL_IS-5 sameAs Q17080008.
- IIL_IS-5 sameAs Q17080008.
- IIL_IS-5 wasDerivedFrom IIL_IS-5?oldid=668399834.
- IIL_IS-5 isPrimaryTopicOf IIL_IS-5.