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Statements

Subject Item
dbr:Renard_R.30
rdf:type
schema:Product yago:Type105840188 wikidata:Q11436 yago:Abstraction100002137 yago:Category105838765 yago:Concept105835747 yago:Kind105839024 owl:Thing yago:Idea105833840 dbo:MeanOfTransportation dbo:Aircraft yago:PsychologicalFeature100023100 yago:Cognition100023271 yago:Content105809192
rdfs:label
Renard R-30 Renard R.30
rdfs:comment
Le Renard R-30 est un avion léger trimoteur resté à l'état de prototype construit par l'avionneur belge Renard Constructions Aéronautiques. The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931. It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment. One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings. Construction was metal throughout, skinned in plywood and fabric.
dct:subject
dbc:Renard_aircraft dbc:1930s_Belgian_airliners dbc:Trimotors dbc:Aircraft_first_flown_in_1931 dbc:High-wing_aircraft
dbo:wikiPageID
21262685
dbo:wikiPageRevisionID
896032687
dbo:wikiPageWikiLink
dbc:High-wing_aircraft dbc:Renard_aircraft dbr:Constructions_Aéronautiques_G._Renard dbc:1930s_Belgian_airliners dbr:Plywood dbc:Trimotors dbc:Aircraft_first_flown_in_1931 dbr:Belgian_Congo dbr:Renard_Type_120
owl:sameAs
n9:3A2B2 freebase:m.05f93mp wikidata:Q3424777 dbpedia-fr:Renard_R-30
dbp:spanM
15
dbp:stallSpeedKmh
95
dbp:timeToAltitude
180.0
dbp:wingAreaSqm
34
n19:m
60.4
dbp:wikiPageUsesTemplate
dbt:Cvt dbt:Cite_book dbt:Infobox_Aircraft_Type dbt:Reflist dbt:Aircraft_specs dbt:Renard_aircraft
dbp:primeUnits%3F_
met
dbp:firstFlight
1931
dbp:nationalOrigin
Belgium
dbp:capacity
6
dbp:crew
1
dbp:manufacturer
dbr:Constructions_Aéronautiques_G._Renard
dbp:ref
Jane's all the World's Aircraft 1931
dbp:type
Airliner
dbo:abstract
The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931. It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment. One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings. Construction was metal throughout, skinned in plywood and fabric. The R.30 was designed in response to a Belgian government requirement of 1929 for a long-range passenger transport aircraft to service Belgian Congo. The design met the specifications laid down, but by the time it flew in 1931, it was judged already obsolete. The single prototype, registered OO-AMK, was the only example built. Le Renard R-30 est un avion léger trimoteur resté à l'état de prototype construit par l'avionneur belge Renard Constructions Aéronautiques.
dbp:ceilingM
6100
dbp:climbRateMs
4.4
dbp:emptyWeightKg
1167
dbp:eng1Hp
120
dbp:eng1Name
dbr:Renard_Type_120
dbp:eng1Note
at 1,750 rpm; at 1900 rpm for take-off
dbp:eng1Number
3
dbp:eng1Type
5
dbp:grossWeightKg
2050
dbp:heightM
3.4
dbp:lengthM
10
dbp:maxSpeedKmh
207
dbp:numberBuilt
1
dbp:propBladeNumber
2
dbp:propDiaM
2.3
dbp:propName
wooden fixed-pitch propellers
dbp:rangeKm
700
gold:hypernym
dbr:Airliner
prov:wasDerivedFrom
wikipedia-en:Renard_R.30?oldid=896032687&ns=0
dbo:wikiPageLength
3698
dbo:numberBuilt
1
dbo:manufacturer
dbr:Constructions_Aéronautiques_G._Renard
foaf:isPrimaryTopicOf
wikipedia-en:Renard_R.30