dbo:abstract |
Agusta A.115 (imatrikulace I-AGUC) byl prototyp italského lehkého vrtulníku, který poprvé vzlétl v roce 1961. Jednalo se v podstatě o s pylonem vyrovnávacího rotoru tvořeným nekrytou trubkovou konstrukcí a poháněný turbohřídelovým motorem . K sériové výrobě nedošlo. (cs) The Agusta A.115 (registration I-AGUC) was a prototype helicopter flown in 1961 in Italy. It was essentially a Bell 47J-3 with an unclad, tubular tail boom, and powered by a Turbomeca Astazou II turboshaft engine. No production ensued. (en) L'Agusta A115 era un elicottero biposto sviluppato come prototipo di maggiore velocità rispetto ai modelli precedenti e in grado comunque di atterrare in spazi limitati.Questo modello fu la risposta italiana alla nascita in america di elicotteri con maggiore autonomia. (it) |
dbo:manufacturer |
dbr:Agusta |
dbo:numberBuilt |
1 (xsd:nonNegativeInteger) |
dbo:predecessor |
dbr:Bell_47J_Ranger |
dbo:thumbnail |
wiki-commons:Special:FilePath/Augusta_a115.png?width=300 |
dbo:type |
dbr:Helicopter |
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10359122 (xsd:integer) |
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3384 (xsd:nonNegativeInteger) |
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dbp:capacity |
3 (xsd:integer) |
dbp:ceilingM |
4750 (xsd:integer) |
dbp:crew |
1 (xsd:integer) |
dbp:cruiseSpeedKmh |
150 (xsd:integer) |
dbp:developedFrom |
dbr:Bell_47J_Ranger |
dbp:emptyWeightKg |
730 (xsd:integer) |
dbp:eng1Hp |
480 (xsd:integer) |
dbp:eng1Name |
Turbomeca Astazou II (en) |
dbp:eng1Number |
1 (xsd:integer) |
dbp:eng1Type |
dbr:Turboshaft |
dbp:firstFlight |
1961 (xsd:integer) |
dbp:grossWeightKg |
1350 (xsd:integer) |
dbp:heightM |
2.940000 (xsd:double) |
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32 (xsd:integer) |
dbp:lengthIn |
6 (xsd:integer) |
dbp:manufacturer |
dbr:Agusta |
dbp:maxSpeedKmh |
170 (xsd:integer) |
dbp:numberBuilt |
1 (xsd:integer) |
dbp:primeUnits?_ |
met (en) |
dbp:rangeKm |
260 (xsd:integer) |
dbp:ref |
Jane's All The World's Aircraft 1961–62 (en) |
dbp:related |
* Bell 47 * Bell 47J Ranger (en) |
dbp:rotAreaSqm |
101 (xsd:integer) |
dbp:rotDiaFt |
37 (xsd:integer) |
dbp:rotDiaIn |
2 (xsd:integer) |
dbp:rotNumber |
1 (xsd:integer) |
dbp:status |
Cancelled (en) |
dbp:type |
Light helicopter (en) |
dbp:wikiPageUsesTemplate |
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dcterms:subject |
dbc:1960s_Italian_helicopters dbc:1970s_Italian_civil_utility_aircraft dbc:Agusta_aircraft dbc:Aircraft_first_flown_in_1961 |
gold:hypernym |
dbr:Helicopter |
rdf:type |
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rdfs:comment |
Agusta A.115 (imatrikulace I-AGUC) byl prototyp italského lehkého vrtulníku, který poprvé vzlétl v roce 1961. Jednalo se v podstatě o s pylonem vyrovnávacího rotoru tvořeným nekrytou trubkovou konstrukcí a poháněný turbohřídelovým motorem . K sériové výrobě nedošlo. (cs) The Agusta A.115 (registration I-AGUC) was a prototype helicopter flown in 1961 in Italy. It was essentially a Bell 47J-3 with an unclad, tubular tail boom, and powered by a Turbomeca Astazou II turboshaft engine. No production ensued. (en) L'Agusta A115 era un elicottero biposto sviluppato come prototipo di maggiore velocità rispetto ai modelli precedenti e in grado comunque di atterrare in spazi limitati.Questo modello fu la risposta italiana alla nascita in america di elicotteri con maggiore autonomia. (it) |
rdfs:label |
Agusta A.115 (cs) Agusta A.115 (en) Agusta A115 (it) |
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freebase:Agusta A.115 wikidata:Agusta A.115 dbpedia-cs:Agusta A.115 dbpedia-fa:Agusta A.115 dbpedia-it:Agusta A.115 http://tg.dbpedia.org/resource/Agusta_A.115 dbpedia-vi:Agusta A.115 https://global.dbpedia.org/id/3KJrP |
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wikipedia-en:Agusta_A.115?oldid=1087300045&ns=0 |
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wiki-commons:Special:FilePath/Augusta_a115.png |
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wikipedia-en:Agusta_A.115 |
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dbr:Bell_47J_Ranger |
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