| dbo:abstract
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- 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)
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| dbo:numberBuilt
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- 1 (xsd:nonNegativeInteger)
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| dbo:origin
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| dbo:predecessor
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| dbo:type
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| dbo:wikiPageID
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| dbo:wikiPageLength
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- 7267 (xsd:nonNegativeInteger)
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| dbo:wikiPageRevisionID
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| dbo:wikiPageWikiLink
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| dbp:airfoil
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- NACA 43015 root, 43012A from mid span outwards (en)
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| dbp:aspectRatio
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| dbp:crew
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| dbp:designer
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| dbp:developedFrom
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| dbp:emptyWeightKg
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| dbp:eng1Hp
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| dbp:eng1Name
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| dbp:eng1Number
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| dbp:firstFlight
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| dbp:glideRatio
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| dbp:grossWeightKg
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| dbp:heightM
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| dbp:lengthM
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| dbp:manufacturer
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- Intreprinderea de industrie Locală (en)
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| dbp:nationalOrigin
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| dbp:neverExceedSpeedKmh
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| dbp:neverExceedSpeedNote
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- placard, in smooth air
*Rough air speed max:
*Aerotow speed: (en)
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| dbp:numberBuilt
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| dbp:primeUnits?_
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| dbp:propBladeNumber
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| dbp:ref
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- Sailplanes of the World, pp.200-1 (en)
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| dbp:sinkRateMs
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| dbp:sinkRateNote
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- minimum, at . Jane's 1962 data give slightly poorer best glide ratio and sink rate, at lower speeds (en)
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| dbp:spanM
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| dbp:stallSpeedKmh
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| dbp:type
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- Single seat motor glider (en)
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| dbp:wikiPageUsesTemplate
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| dbp:wingAreaSqm
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| dbp:wingLoadingKg/m
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| dcterms:subject
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| rdf:type
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| rdfs:comment
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- 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)
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| rdfs:label
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| owl:sameAs
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| prov:wasDerivedFrom
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| foaf:isPrimaryTopicOf
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| is dbo:wikiPageWikiLink
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| is foaf:primaryTopic
of | |
