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n7http://commons.wikimedia.org/wiki/Special:FilePath/H_IIA_No._F23_with_GPM_on_its_way_to_the_launchpad.
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Subject Item
dbpedia:H-IIA
rdfs:comment
H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch an interplanetary space probe to Venus. Launches occur at the Tanegashima Space Center.
foaf:name
H-IIA
foaf:depiction
n7:jpg
dbpedia-owl:countryOrigin
dbpedia:Japan
dbpedia-owl:diameter
4.0
dbpedia-owl:failedLaunches
1
dbpedia-owl:height
53.0
dbpedia-owl:launchSite
dbpedia:Tanegashima dbpedia:Yoshinobu_Launch_Complex
dbpedia-owl:maidenFlight
2001-08-29Z 2006-12-18Z 2002-02-04Z 2005-02-26Z
dbpedia-owl:manufacturer
dbpedia:Mitsubishi_Heavy_Industries dbpedia:Alliant_Techsystems
dbpedia-owl:rocketFunction
dbpedia:Launch_vehicle
dbpedia-owl:rocketStages
2
dbpedia-owl:status
Active
dbpedia-owl:successfulLaunches
27 202
dbpedia-owl:thumbnail
n4:300
dbpedia-owl:totalLaunches
202 28