{ "items" : [
    { "id" : "http://dbpedia.org/resource/Saturn_C-4"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Saturn C-4 was the fourth rocket in the Saturn C series studied from 1959 to 1962. The C-4 design was proposed in 1960 for a three-stage launch vehicle that could launch 99,000 kg (218,000 lb) to Low Earth orbit and send 32,000 kg (70,000 lb) to the Moon via Trans-lunar injection.  It met the initial requirements for a lunar orbit rendezvous and lunar landing mission.It would have consisted of three stages; an S-IB-4 first stage, a S-II-4 second stage and a S-IVB third stage." ] ,
        "http://xmlns.com/foaf/0.1/name" : [ "Saturn C-4" ] ,
        "http://dbpedia.org/ontology/comparable" : [ "http://dbpedia.org/resource/Saturn_V" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 8.128 ] ,
        "http://dbpedia.org/ontology/height" : [ 81.99120000000001 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37" ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Douglas_Aircraft_Company",
          "http://dbpedia.org/resource/North_American_Aviation",
          "http://dbpedia.org/resource/Boeing" ] ,
        "http://dbpedia.org/ontology/mass" : [ 464336712 ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Moon",
          "http://dbpedia.org/resource/Low_Earth_orbit" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 3 ] ,
        "http://dbpedia.org/ontology/status" : [ "Proposed (1962)"] } } }
