{ "items" : [
    { "id" : "http://dbpedia.org/resource/Saturn_INT-20"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage.Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five." ] ,
        "http://xmlns.com/foaf/0.1/name" : [ "Saturn INT-20" ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/INT20C.svg" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 10 ] ,
        "http://dbpedia.org/ontology/height" : [ 85 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Kennedy_Space_Center_Launch_Complex_39" ] ,
        "http://dbpedia.org/ontology/lowerEarthOrbitPayload" : [ 60500000 ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Douglas_Aircraft_Company",
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        "http://dbpedia.org/ontology/mass" : [ 2304000000 ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Low_Earth_orbit" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 2 ] ,
        "http://dbpedia.org/ontology/status" : [ "Proposal" ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/INT20C.svg?width=300"] } } }
