{ "items" : [
    { "id" : "http://dbpedia.org/resource/Delta_A"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Delta A, or Thor-Delta A was an American expendable launch system used to launch two Explorer spacecraft in October 1962. A derivative of the Thor-Delta, it was a member of the Delta family of rockets.The first stage was a Thor missile in the DM-21 configuration, and the second stage was the Delta A, an uprated version of the original Delta. An Altair solid rocket motor was used as a third stage." ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Thor_Delta_A_with_Explorer_14_(Oct._2,_1962).gif" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/United_States" ] ,
        "http://dbpedia.org/ontology/finalFlight" : [ "1962-10-27Z" ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Cape_Canaveral_Air_Force_Station" ] ,
        "http://dbpedia.org/ontology/maidenFlight" : [ "1962-10-02Z" ] ,
        "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/Thor_Delta_A_with_Explorer_14_(Oct._2,_1962).gif?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 2] } } }
