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      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#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." ] ,
        "http://xmlns.com/foaf/0.1/name" : [ "H-IIA" ] ,
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        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/Japan" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 4 ] ,
        "http://dbpedia.org/ontology/failedLaunches" : [ 1 ] ,
        "http://dbpedia.org/ontology/height" : [ 53 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Tanegashima",
          "http://dbpedia.org/resource/Yoshinobu_Launch_Complex" ] ,
        "http://dbpedia.org/ontology/maidenFlight" : [ "2001-08-29Z",
          "2006-12-18Z",
          "2002-02-04Z",
          "2005-02-26Z" ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Mitsubishi_Heavy_Industries",
          "http://dbpedia.org/resource/Alliant_Techsystems" ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Launch_vehicle" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 2 ] ,
        "http://dbpedia.org/ontology/status" : [ "Active" ] ,
        "http://dbpedia.org/ontology/successfulLaunches" : [ 27,
          202 ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/H_IIA_No._F23_with_GPM_on_its_way_to_the_launchpad.jpg?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 202,
          28] } } }
