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n8http://commons.wikimedia.org/wiki/Special:FilePath/Thor-Able_II_Transit_1A.
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Subject Item
dbpedia:Thor-Able
rdfs:comment
The Thor-Able was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960. It was a two stage rocket, consisting of a Thor IRBM as a first stage, and a Vanguard-derived Able second stage. On some flights, an Altair solid rocket motor was added as a third stage. It was a member of the Thor family, and an early predecessor of the Delta.
foaf:depiction
n8:jpg
dbpedia-owl:comparable
n4:
dbpedia-owl:countryOrigin
dbpedia:United_States
dbpedia-owl:diameter
2.44
dbpedia-owl:failedLaunches
6
dbpedia-owl:finalFlight
1960-04-01Z
dbpedia-owl:height
26.9
dbpedia-owl:launchSite
dbpedia:Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17 dbpedia:Cape_Canaveral_Air_Force_Station
dbpedia-owl:maidenFlight
1958-04-24Z
dbpedia-owl:manufacturer
dbpedia:Aerojet dbpedia:Douglas_Aircraft_Company
dbpedia-owl:mass
5.1608e+07
dbpedia-owl:rocketFunction
dbpedia:Sounding_rocket dbpedia:Expendable_launch_system
dbpedia-owl:rocketStages
2
dbpedia-owl:successfulLaunches
10
dbpedia-owl:successor
dbpedia:Thor-Ablestar n9:
dbpedia-owl:thumbnail
n5:300
dbpedia-owl:totalLaunches
16