{ "items" : [
    { "id" : "http://dbpedia.org/resource/N-II_(rocket)"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#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." ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/N-II.svg" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 2.44 ] ,
        "http://dbpedia.org/ontology/finalFlight" : [ "1987-02-19Z" ] ,
        "http://dbpedia.org/ontology/height" : [ 35 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Tanegashima" ] ,
        "http://dbpedia.org/ontology/maidenFlight" : [ "1981-02-11Z" ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/McDonnell_Douglas",
          "http://dbpedia.org/resource/Mitsubishi_Heavy_Industries" ] ,
        "http://dbpedia.org/ontology/mass" : [ 132690000 ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Launch_vehicle" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 2,
          3 ] ,
        "http://dbpedia.org/ontology/status" : [ "Retired" ] ,
        "http://dbpedia.org/ontology/successfulLaunches" : [ 8 ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/N-II.svg?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 8] } } }
