| http://dbpedia.org/ontology/abstract
|
The Thor T/A is a Canadian ultralight aircraft that was designed by Thorsten B. Strenger (or possibly Gunter Webster) and produced by of Weston, Ontario. The aircraft was supplied as a kit for amateur construction.
|
| http://dbpedia.org/ontology/manufacturer
|
http://dbpedia.org/resource/Thor_Air +
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|
http://dbpedia.org/resource/Canada +
|
| http://dbpedia.org/ontology/type
|
http://dbpedia.org/resource/Ultralight_aircraft +
|
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|
34258386
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5587
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|
1067227457
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|
http://dbpedia.org/resource/Rotax_447 +
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, http://dbpedia.org/resource/Category:Homebuilt_aircraft +
, http://dbpedia.org/resource/FAR_103_Ultralight_Vehicles +
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, http://dbpedia.org/resource/Elevator_%28aircraft%29 +
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, http://dbpedia.org/resource/Rotax_277 +
, http://dbpedia.org/resource/Strut-braced +
, http://dbpedia.org/resource/Tractor_configuration +
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| http://dbpedia.org/property/ceilingFt
|
10000
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| http://dbpedia.org/property/climbRateFtmin
|
700
|
| http://dbpedia.org/property/crew
|
one
|
| http://dbpedia.org/property/cruiseSpeedMph
|
55
|
| http://dbpedia.org/property/designer
|
Thorsten B. Strenger
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238
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28
|
| http://dbpedia.org/property/eng1Name
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http://dbpedia.org/resource/Rotax_277 +
|
| http://dbpedia.org/property/eng1Number
|
1
|
| http://dbpedia.org/property/eng1Type
|
single cylinder, two-stroke aircraft engine
|
| http://dbpedia.org/property/gLimits
|
+3/-2
|
| http://dbpedia.org/property/glideRatio
|
9
|
| http://dbpedia.org/property/grossWeightLb
|
500
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| http://dbpedia.org/property/heightFt
|
7
|
| http://dbpedia.org/property/heightIn
|
8
|
| http://dbpedia.org/property/introduced
|
1985
|
| http://dbpedia.org/property/lengthFt
|
13.8
|
| http://dbpedia.org/property/manufacturer
|
http://dbpedia.org/resource/Thor_Air +
|
| http://dbpedia.org/property/maxSpeedMph
|
63
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| http://dbpedia.org/property/nationalOrigin
|
http://dbpedia.org/resource/Canada +
|
| http://dbpedia.org/property/primeUnits%3F
|
imp
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| http://dbpedia.org/property/ref
|
Cliche and the Virtual Ultralight Museum
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| http://dbpedia.org/property/spanFt
|
32
|
| http://dbpedia.org/property/spanIn
|
4
|
| http://dbpedia.org/property/stallSpeedMph
|
22
|
| http://dbpedia.org/property/status
|
Production completed
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| http://dbpedia.org/property/type
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http://dbpedia.org/resource/Ultralight_aircraft +
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|
| http://dbpedia.org/property/wingAreaSqft
|
167
|
| http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:Single-engined_tractor_aircraft +
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|
| http://purl.org/linguistics/gold/hypernym
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http://dbpedia.org/resource/Aircraft +
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| http://www.w3.org/ns/prov#wasDerivedFrom
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|
| rdfs:comment |
The Thor T/A is a Canadian ultralight aircraft that was designed by Thorsten B. Strenger (or possibly Gunter Webster) and produced by of Weston, Ontario. The aircraft was supplied as a kit for amateur construction.
|
| rdfs:label |
Thor T/A
|
