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About: Delta E     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : umbel-rc:RocketEngine, within Data Space : dbpedia.org:8891 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 E, or Thor-Delta E was an American expendable launch system used for twenty-three orbital launches between 1965 and 1971. It was a member of the Delta family of rockets. The first stage was a Thor missile in the DSV-2C configuration, and the second stage was the Delta-E, which was derived from the earlier Delta-A. Three Castor-1 solid rocket boosters were clustered around the first stage. Two different solid-fuel upper stages were available; an Altair-2 was used on the baseline version, however this could be replaced with an to increase performance. A Delta E with the FW-4D upper stage was designated Delta E1. Six flights used the Delta E configuration and seventeen used the Delta E1.