{ "items" : [
    { "id" : "http://dbpedia.org/resource/Saturn_C-2"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection.The C-2 design concept was for a proposed manned circumlunar flight and the Earth orbit rendezvous (EOR) missions.  It was initially considered for the Apollo lunar landing at the earliest possible date (1967)." ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 6.52272 ] ,
        "http://dbpedia.org/ontology/height" : [ 68.45808 ] ,
        "http://dbpedia.org/ontology/mass" : [ 620071200 ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Launch_vehicle",
          "http://dbpedia.org/resource/Apollo_program" ] ,
        "http://dbpedia.org/ontology/status" : [ "Study, not developed"] } } }
