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Statements

Subject Item
dbpedia:Dassault_Balzac_V
rdf:type
yago:Instrumentality103575240 yago:Vehicle104524313 yago:Craft103125870 yago:Conveyance103100490 yago:Aircraft102686568 owl:Thing n13:Model_airplane dbpedia-owl:MeanOfTransportation n13:TransportationDevice_Vehicle yago:Whole100003553 schema:Product yago:PhysicalEntity100001930 yago:Object100002684 schema:CreativeWork n19:DesignedArtifact n20:Q11436 dbpedia-owl:MilitaryConflict yago:Artifact100021939 dbpedia-owl:Aircraft
rdfs:label
Dassault Balzac V バルザック V (航空機) Dassault Balzac V Dassault Balzac V
rdfs:comment
Dassault Balzac V – francuski doświadczalny samolot pionowego startu i pionowego lądowania zbudowany na bazie maszyny Dassault Mirage III. Konstrukcja posłużyła do przetestowania rozwiązań konstrukcyjnych jakie miały zostać użyte w seryjnym samolocie Dassault Mirage III V. Die Dassault Balzac V (V für Vertikal) war ein Experimentalflugzeug des französischen Flugzeugherstellers Dassault Aviation, das senkrecht starten und landen konnte (VTOL). Es wurde als Überschallflugzeug mit einer Hub- und Schubtriebwerkskonfiguration (lift + cruise) ausgelegt. バルザック V(Balzac V)は、フランスの垂直離着陸機。ミラージュIII Vの試験・研究機という位置づけであり、垂直離着陸機による亜音速飛行が主たる目的であった。 The Dassault Balzac V was a French vertical takeoff and landing (VTOL) testbed of the early 1960s. It was built by Dassault Aviation from a prototype Mirage III aircraft to test the configuration for the Mirage IIIV. The sole example was badly damaged during its second flight test accident and was not repaired.
owl:sameAs
fbase:m.04_1rc0 n21:this dbpedia:Dassault_Balzac_V n22:Dassault_Balzac_V n23:Q1781734 n20:Q1781734 n24:Dassault_Balzac_V n25:バルザック_V_(航空機) n26:Dassault_Balzac_V
foaf:topic
dbpedia:Dassault_Mirage_IIIV dbpedia:Balzac_(disambiguation) dbpedia:Balzac_V dbpedia:Dassault_Balzac dbpedia:Dassault_Balzac_Mirage_IIIV n5:Dassault_Balzac_V
dcterms:subject
category:VTOL_aircraft category:Dassault_Group_aircraft category:French_fighter_aircraft_1960–1969 category:Tailless_delta-wing_aircraft
foaf:isPrimaryTopicOf
n5:Dassault_Balzac_V
schema:url
dbpedia:Dassault_Balzac_V
schema:mainEntity
n11:Dassault_Balzac_V
void:sparqlEndpoint
n29:
dbpprop:lists
* List of military aircraft of France * List of fighter aircraft * List of VTOL aircraft
dbpprop:related
* Dassault Mirage III * Dassault Mirage IIIV
dbpprop:similarAircraft
* EWR VJ 101 * Hawker Siddeley Harrier * Hawker P.1154 * Rockwell XFV-12 * Yakovlev Yak-38 * Yakovlev Yak-141
dbpprop:crew
one
dbpprop:maxSpeedMore
at sea level
n18:weight
1.12
dbpprop:numberOfJets
1
dbpprop:thrustAlt
4850
dbpprop:thrustMain
21.57 kN
dbpprop:typeOfJet
Cruise turbojet
n27:hypernym
dbpedia:Landing
dbpedia-owl:abstract
バルザック V(Balzac V)は、フランスの垂直離着陸機。ミラージュIII Vの試験・研究機という位置づけであり、垂直離着陸機による亜音速飛行が主たる目的であった。 The Dassault Balzac V was a French vertical takeoff and landing (VTOL) testbed of the early 1960s. It was built by Dassault Aviation from a prototype Mirage III aircraft to test the configuration for the Mirage IIIV. The sole example was badly damaged during its second flight test accident and was not repaired. Die Dassault Balzac V (V für Vertikal) war ein Experimentalflugzeug des französischen Flugzeugherstellers Dassault Aviation, das senkrecht starten und landen konnte (VTOL). Es wurde als Überschallflugzeug mit einer Hub- und Schubtriebwerkskonfiguration (lift + cruise) ausgelegt. Dassault Balzac V – francuski doświadczalny samolot pionowego startu i pionowego lądowania zbudowany na bazie maszyny Dassault Mirage III. Konstrukcja posłużyła do przetestowania rozwiązań konstrukcyjnych jakie miały zostać użyte w seryjnym samolocie Dassault Mirage III V.
dbpedia-owl:manufacturer
dbpedia:Dassault_Aviation
dbpedia-owl:numberBuilt
1
dbpedia-owl:predecessor
dbpedia:Dassault_Mirage_III
dbpedia-owl:productionEndYear
1962-01-01
dbpedia-owl:productionStartYear
1962-01-01
dbpedia-owl:type
dbpedia:VTOL
dbpedia-owl:wikiPageExternalLink
n14:DassaultBalzacV.htm
dbpedia-owl:wikiPageID
15364428
dbpedia-owl:wikiPageRevisionID
739675875
prov:wasDerivedFrom
n5:Dassault_Balzac_V?oldid=739675875
dbpprop:emptyWeightAlt
13500.0
dbpprop:emptyWeightMain
6124.0
dbpprop:engine(jet)_
Bristol Siddeley Orpheus BOr 3
dbpprop:heightAlt
m 15 ft
dbpprop:heightMain
4.6
dbpprop:lengthAlt
42
dbpprop:lengthMain
13.1 m
dbpprop:loadedWeightAlt
15432.0
dbpprop:loadedWeightMain
7000.0
dbpprop:spanAlt
23
dbpprop:spanMain
7.3 m
dbpprop:firstFlight
1962-10-13
dbpprop:primaryUser
dbpedia:French_Air_Force
dbpprop:areaAlt
292.78
dbpprop:areaMain
27.2
dbpprop:loadingAlt
52.700000000000003
dbpprop:loadingMain
257.300000000000011
dbpprop:engine(prop)_
dbpedia:Rolls-Royce_RB108
dbpprop:jetOrProp%3F_
both
dbpprop:maxSpeedAlt
686.0
dbpprop:maxSpeedMain
1104.0
dbpprop:morePerformance
900.0
dbpprop:numberOfProps
8
dbpprop:planeOrCopter%3F_
plane
dbpprop:powerAlt
2160
dbpprop:powerMain
9.6 kN
dbpprop:typeOfProp
lift turbojet