{ "items" : [
    { "id" : "http://dbpedia.org/resource/M-V"
      "properties" : {
        "http://www.w3.org/2000/01/rdf-schema#comment" : [ "The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in 1990 at a cost of 15 billion yen. It has three stages and is 30.7 meters high, 2.5 meters in diameter, and weighs about 140 tonnes (310,000 pounds)." ] ,
        "http://xmlns.com/foaf/0.1/name" : [ "M-V" ] ,
        "http://xmlns.com/foaf/0.1/depiction" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/M-V_launching_ASTRO-E2.jpeg" ] ,
        "http://dbpedia.org/ontology/countryOrigin" : [ "http://dbpedia.org/resource/Japan" ] ,
        "http://dbpedia.org/ontology/diameter" : [ 2.5 ] ,
        "http://dbpedia.org/ontology/failedLaunches" : [ 1 ] ,
        "http://dbpedia.org/ontology/finalFlight" : [ "2006-09-22Z",
          "2003-05-09Z" ] ,
        "http://dbpedia.org/ontology/height" : [ 30.8 ] ,
        "http://dbpedia.org/ontology/launchSite" : [ "http://dbpedia.org/resource/Kagoshima" ] ,
        "http://dbpedia.org/ontology/lowerEarthOrbitPayload" : [ 1800000 ] ,
        "http://dbpedia.org/ontology/maidenFlight" : [ "1997-02-12Z",
          "2000-02-10Z" ] ,
        "http://dbpedia.org/ontology/manufacturer" : [ "http://dbpedia.org/resource/Nissan" ] ,
        "http://dbpedia.org/ontology/rocketFunction" : [ "http://dbpedia.org/resource/Solid-fuel_rocket" ] ,
        "http://dbpedia.org/ontology/rocketStages" : [ 4,
          3 ] ,
        "http://dbpedia.org/ontology/status" : [ "Retired" ] ,
        "http://dbpedia.org/ontology/successfulLaunches" : [ 6 ] ,
        "http://dbpedia.org/ontology/thumbnail" : [ "http://commons.wikimedia.org/wiki/Special:FilePath/M-V_launching_ASTRO-E2.jpeg?width=300" ] ,
        "http://dbpedia.org/ontology/totalLaunches" : [ 7] } } }
