This HTML5 document contains 21 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

PrefixNamespace IRI
dbpedia-owlhttp://dbpedia.org/ontology/
foafhttp://xmlns.com/foaf/0.1/
rdfshttp://www.w3.org/2000/01/rdf-schema#
n7http://commons.wikimedia.org/wiki/Special:FilePath/H-ii_adeos.
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
xsdhhttp://www.w3.org/2001/XMLSchema#
n6http://commons.wikimedia.org/wiki/Special:FilePath/H-ii_adeos.gif?width=
dbpediahttp://dbpedia.org/resource/
Subject Item
dbpedia:H-II
rdfs:comment
The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.
foaf:name
H-II
foaf:depiction
n7:gif
dbpedia-owl:countryOrigin
dbpedia:Japan
dbpedia-owl:diameter
4.0
dbpedia-owl:failedLaunches
1
dbpedia-owl:finalFlight
1999-11-15Z
dbpedia-owl:height
49.0
dbpedia-owl:launchSite
dbpedia:Tanegashima_Space_Center dbpedia:Yoshinobu_Launch_Complex
dbpedia-owl:lowerEarthOrbitPayload
1.006e+07
dbpedia-owl:maidenFlight
1994-02-03Z
dbpedia-owl:manufacturer
dbpedia:Mitsubishi_Heavy_Industries
dbpedia-owl:mass
2.6e+08
dbpedia-owl:partialFailedLaunches
1
dbpedia-owl:rocketFunction
dbpedia:Launch_vehicle
dbpedia-owl:rocketStages
2
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
5
dbpedia-owl:thumbnail
n6:300
dbpedia-owl:totalLaunches
7