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About: Delta C     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : umbel-rc:RocketEngine, within Data Space : dbpedia.org associated with source document(s)

Type: Thingmean of transportationRocketrocketyago:Artifact100021939yago:Conveyance103100490yago:Instrumentality103575240yago:Object100002684yago:PhysicalEntity100001930yago:Rocket104099429yago:Vehicle104524313yago:Whole100003553umbel-rc:RocketEngine New Facet based on Instances of this Class

The Delta C, or Thor-Delta C was an American expendable launch system used for thirteen orbital launches between 1963 and 1969. It was a member of the Delta family of rockets. The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the , which was derived from the earlier . The baseline Delta C used an Altair-2 third stage, whilst the Delta C1 had an third stage, which provided a higher payload capacity than the Altair. It is unclear whether two or three launches were made using the C1 configuration.