{ "items" : [
    { "id" : "http://dbpedia.org/resource/Delta_D"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Delta D, Thrust Augmented Delta or Thor-Delta D was an American expendable launch system used to launch two communications satellites in 1964 and 1965. It was derived from the Delta C, and was a member of the Delta family of rockets.The three-stage core vehicle was essentially the same as the Delta C. The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the Delta D, which was derived from the earlier Delta. An Altair-2 SRM was used as a third stage." ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Delta_D_Intelsat1.jpg" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/finalFlight" : [ "1965-04-06Z" ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Cape_Canaveral_Air_Force_Station" ] ,
        "http://dbpedia.org/ontology/maidenFlight" : [ "1964-08-19Z" ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Expendable_launch_system" ] ,
        "http://dbpedia.org/ontology/status" : [ "Retired" ] ,
        "http://dbpedia.org/ontology/successfulLaunches" : [ 2 ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Delta_D_Intelsat1.jpg?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 2] } } }
