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n6http://commons.wikimedia.org/wiki/Special:FilePath/Atlas_III_Centaur.
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Subject Item
dbpedia:Atlas_III
rdfs:comment
The Lockheed Martin Atlas III was an American orbital launch vehicle, used between 2000 and 2005. It was the first member of the Atlas family since the Atlas A to feature a "normal" staging method, compared to the previous Atlas family members, which were equipped with jettisonable engines on the first (sustainer) stage.
foaf:name
Atlas III
foaf:depiction
n6:jpg
dbpedia-owl:countryOrigin
dbpedia:United_States
dbpedia-owl:diameter
3.05
dbpedia-owl:finalFlight
2004-03-13Z 2005-02-03Z
dbpedia-owl:height
52.8
dbpedia-owl:launchSite
dbpedia:Spaceport_Florida_Launch_Complex_36 dbpedia:Cape_Canaveral_Air_Force_Station
dbpedia-owl:lowerEarthOrbitPayload
8.64e+06 1.0218e+07
dbpedia-owl:maidenFlight
2002-02-21Z 2000-05-24Z
dbpedia-owl:manufacturer
dbpedia:Lockheed_Martin
dbpedia-owl:mass
2.14338e+08
dbpedia-owl:rocketFunction
dbpedia:Launch_vehicle
dbpedia-owl:rocketStages
2
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
6 2
dbpedia-owl:thumbnail
n7:300
dbpedia-owl:totalLaunches
6 2