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PrefixNamespace IRI
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foafhttp://xmlns.com/foaf/0.1/
rdfshttp://www.w3.org/2000/01/rdf-schema#
n7http://commons.wikimedia.org/wiki/Special:FilePath/M-V_launching_ASTRO-E2.
n5http://commons.wikimedia.org/wiki/Special:FilePath/M-V_launching_ASTRO-E2.jpeg?width=
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
xsdhhttp://www.w3.org/2001/XMLSchema#
dbpediahttp://dbpedia.org/resource/
Subject Item
dbpedia:M-V
rdfs:comment
The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in 1990 at a cost of 15 billion yen. It has three stages and is 30.7 meters high, 2.5 meters in diameter, and weighs about 140 tonnes (310,000 pounds).
foaf:name
M-V
foaf:depiction
n7:jpeg
dbpedia-owl:countryOrigin
dbpedia:Japan
dbpedia-owl:diameter
2.5
dbpedia-owl:failedLaunches
1
dbpedia-owl:finalFlight
2006-09-22Z 2003-05-09Z
dbpedia-owl:height
30.8
dbpedia-owl:launchSite
dbpedia:Kagoshima
dbpedia-owl:lowerEarthOrbitPayload
1.8e+06
dbpedia-owl:maidenFlight
1997-02-12Z 2000-02-10Z
dbpedia-owl:manufacturer
dbpedia:Nissan
dbpedia-owl:rocketFunction
dbpedia:Solid-fuel_rocket
dbpedia-owl:rocketStages
4 3
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
6
dbpedia-owl:thumbnail
n5:300
dbpedia-owl:totalLaunches
7