{ "items" : [
    { "id" : "http://dbpedia.org/resource/Hawker_Siddeley_P.1154"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The Hawker Siddeley P.1154 was a planned supersonic vertical/short take-off and landing (V/STOL) fighter aircraft designed by Hawker Siddeley Aviation (HSA). Developed alongside the subsonic and smaller Hawker Siddeley P.1127/Kestrel, the P.1154 was derived from the P.1150. The P.1150 proposal did not meet NATO Basic Military Requirement 3 and, consequently, the P.1154 was born. This Mach 2-capable platform retained plenum chamber burning previously designed for the P.1150." ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Mirage_III_V_01_Musee_du_Bourget_P1020107.JPG" ] ,
        "http://dbpedia.org/ontology/designer" : [ "http://dbpedia.org/resource/Ralph_Hooper" ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Hawker_Siddeley" ] ,
        "http://dbpedia.org/ontology/predecessor" : [ "http://dbpedia.org/resource/Hawker_Siddeley_P.1127" ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/Mirage_III_V_01_Musee_du_Bourget_P1020107.JPG?width=300" ] ,
        "http://dbpedia.org/ontology/type" : [ "http://dbpedia.org/resource/V/STOL"] } } }
