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PrefixNamespace IRI
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Subject Item
dbpedia:Delta_D
rdfs:comment
The Delta D, Thrust Augmented Delta or Thor-Delta D was an American expendable launch system used to launch two communications satellites in 1964 and 1965. It was derived from the Delta C, and was a member of the Delta family of rockets.The three-stage core vehicle was essentially the same as the Delta C. The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the Delta D, which was derived from the earlier Delta. An Altair-2 SRM was used as a third stage.
foaf:depiction
n7:jpg
dbpedia-owl:countryOrigin
dbpedia:United_States
dbpedia-owl:finalFlight
1965-04-06Z
dbpedia-owl:launchSite
dbpedia:Cape_Canaveral_Air_Force_Station
dbpedia-owl:maidenFlight
1964-08-19Z
dbpedia-owl:rocketFunction
dbpedia:Expendable_launch_system
dbpedia-owl:status
Retired
dbpedia-owl:successfulLaunches
2
dbpedia-owl:thumbnail
n4:300
dbpedia-owl:totalLaunches
2