{ "items" : [
    { "id" : "http://dbpedia.org/resource/Saturn_II"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Saturn II was a series of proposed American Expendable launch vehicles, proposed by North American Aviation in 1966, derived from the Saturn V rocket that was used for the Apollo lunar program. It was, essentially, a version of the Saturn V with the lowest stage removed, producing a two-stage design with a payload intermediate between the Saturn IB and V, delivering about 46,000 pounds (21,000 kg) to low earth orbit." ] ,
        "http://xmlns.com/foaf/0.1/name" : [ "Saturn II" ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Saturn_II.svg" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 10.0584 ] ,
        "http://dbpedia.org/ontology/height" : [ 50.9016 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Kennedy_Space_Center_Launch_Complex_39" ] ,
        "http://dbpedia.org/ontology/lowerEarthOrbitPayload" : [ 21319200 ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Douglas_Aircraft_Company",
          "http://dbpedia.org/resource/North_American_Aviation" ] ,
        "http://dbpedia.org/ontology/mass" : [ 328406400 ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Launch_vehicle" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 2 ] ,
        "http://dbpedia.org/ontology/status" : [ "Cancelled",
          "1967 Study" ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Saturn_II.svg?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 0] } } }
