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|
The IIL IS-12 was a two-seat glider, desig … 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. IS-13a, a version with an all-metal wing.
|
| http://dbpedia.org/ontology/designer
|
http://dbpedia.org/resource/Iosif_%C8%98ilimon +
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| http://dbpedia.org/ontology/numberBuilt
|
1
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| http://dbpedia.org/ontology/origin
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http://dbpedia.org/resource/Romania +
|
| http://dbpedia.org/ontology/type
|
http://dbpedia.org/resource/Training_aircraft +
|
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|
41685612
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|
8226
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|
993033790
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| http://dbpedia.org/ontology/wikiPageWikiLink
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http://dbpedia.org/resource/Wing_tip +
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, http://dbpedia.org/resource/Trailing_edge +
, http://dbpedia.org/resource/Balanced_rudder +
, http://dbpedia.org/resource/Fin +
, http://dbpedia.org/resource/NACA_airfoil +
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, http://dbpedia.org/resource/Glider_%28sailplane%29 +
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|
| http://dbpedia.org/property/airfoil
|
NACA 43015 root, 43012A tip
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| http://dbpedia.org/property/aspectRatio
|
12.5
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| http://dbpedia.org/property/crew
|
Two
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|
http://dbpedia.org/resource/Iosif_%C8%98ilimon +
|
| http://dbpedia.org/property/emptyWeightKg
|
290
|
| http://dbpedia.org/property/firstFlight
|
"1960-12-23"^^xsd:date
|
| http://dbpedia.org/property/gLimits
|
+5/-3
|
| http://dbpedia.org/property/glideRatio
|
best 24 at
|
| http://dbpedia.org/property/grossWeightKg
|
480
|
| http://dbpedia.org/property/lengthM
|
7.6
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| http://dbpedia.org/property/manufacturer
|
Întreprinderea de industrie Locală
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| http://dbpedia.org/property/nationalOrigin
|
http://dbpedia.org/resource/Romania +
|
| http://dbpedia.org/property/neverExceedSpeedKmh
|
200
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| http://dbpedia.org/property/neverExceedSpeedNote
|
placard, in smooth air
*Rough air speed max:
*Aerotow speed:
*Winch launch speed:
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| http://dbpedia.org/property/numberBuilt
|
1
|
| http://dbpedia.org/property/primeUnits%3F
|
met
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| http://dbpedia.org/property/ref
|
Sailplanes of the World, pp. 206–7
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| http://dbpedia.org/property/sinkRateMs
|
0.92
|
| http://dbpedia.org/property/sinkRateNote
|
minimum, at
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| http://dbpedia.org/property/spanM
|
15
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| http://dbpedia.org/property/stallSpeedKmh
|
58
|
| http://dbpedia.org/property/type
|
Experimental two seat trainer glider
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http://dbpedia.org/resource/Template:Iosif_Silimon_aircraft +
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, http://dbpedia.org/resource/Template:Reflist +
|
| http://dbpedia.org/property/wingAreaSqm
|
18
|
| http://dbpedia.org/property/wingLoadingKg/m
|
26.6
|
| http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:1960s_Romanian_sailplanes +
|
| http://purl.org/linguistics/gold/hypernym
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http://dbpedia.org/resource/Glider +
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http://en.wikipedia.org/wiki/IIL_IS-12?oldid=993033790&ns=0 +
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http://en.wikipedia.org/wiki/IIL_IS-12 +
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https://global.dbpedia.org/id/fpmS +
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http://dbpedia.org/ontology/Aircraft +
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|
| rdfs:comment |
The IIL IS-12 was a two-seat glider, desig … 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. IS-13a, a version with an all-metal wing.
|
| rdfs:label |
IIL IS-12
|
