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PrefixNamespace IRI
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foafhttp://xmlns.com/foaf/0.1/
rdfshttp://www.w3.org/2000/01/rdf-schema#
n6http://commons.wikimedia.org/wiki/Special:FilePath/Foguete_VS_40.
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
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dbpediahttp://dbpedia.org/resource/
Subject Item
dbpedia:VS-40
rdfs:comment
The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.This configuration corresponds to the upper stages of the VLS-1 rocket.
foaf:name
VS-40 (Foguete Suborbital VS-40)
foaf:depiction
n6:jpg
dbpedia-owl:countryOrigin
dbpedia:Brazil
dbpedia-owl:diameter
1.01
dbpedia-owl:failedLaunches
0
dbpedia-owl:height
9.5
dbpedia-owl:launchSite
dbpedia:Andøya_Space_Center dbpedia:Alcântara_Launch_Center dbpedia:Barreira_do_Inferno_Launch_Center
dbpedia-owl:lowerEarthOrbitPayload
500000.0
dbpedia-owl:maidenFlight
1993-04-02Z
dbpedia-owl:manufacturer
dbpedia:Instituto_de_Aeronáutica_e_Espaço
dbpedia-owl:mass
6.8e+06
dbpedia-owl:rocketFunction
dbpedia:Sounding_rocket
dbpedia-owl:rocketStages
2
dbpedia-owl:status
Active
dbpedia-owl:thumbnail
n5:300
dbpedia-owl:totalLaunches
3