This HTML5 document contains 17 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/
n2http://dbpedia.org/resource/N-II_(rocket)
rdfshttp://www.w3.org/2000/01/rdf-schema#
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
n5http://commons.wikimedia.org/wiki/Special:FilePath/N-II.svg?width=
n8http://commons.wikimedia.org/wiki/Special:FilePath/N-II.
xsdhhttp://www.w3.org/2001/XMLSchema#
dbpediahttp://dbpedia.org/resource/
Subject Item
n2:
rdfs:comment
The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Delta-F second stage, nine Castor SRMs, and on most flights either a Star-37E or Burner-2 upper stage, identical to the US Delta 0100 series configurations. Eight were launched between 1981 and 1987, before it was replaced by the H-I, which featured Japanese-produced upper stages. All eight launches were successful.
foaf:depiction
n8:svg
dbpedia-owl:diameter
2.44
dbpedia-owl:finalFlight
1987-02-19Z
dbpedia-owl:height
35.0
dbpedia-owl:launchSite
dbpedia:Tanegashima
dbpedia-owl:maidenFlight
1981-02-11Z
dbpedia-owl:manufacturer
dbpedia:McDonnell_Douglas dbpedia:Mitsubishi_Heavy_Industries
dbpedia-owl:mass
1.3269e+08
dbpedia-owl:rocketFunction
dbpedia:Launch_vehicle
dbpedia-owl:rocketStages
2 3
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
8
dbpedia-owl:thumbnail
n5:300
dbpedia-owl:totalLaunches
8