About: Delta E

An Entity of Type: rocket, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

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.

Property Value
dbo:abstract
  • 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. Delta E rockets were launched from Cape Canaveral Air Force Station Launch Complex 17 and Vandenberg Air Force Base Space Launch Complex 2E. All 23 flights were successful. On December 16 1965, a Delta E launched the Pioneer 6 space probe. (en)
  • Thor Delta E – amerykańska rakieta nośna z rodziny Thor Delta. Istniały jej dwa warianty: E (6 startów) i E1 (17 startów). Obydwie wersje wykorzystywały centralny człon i dopalacze na paliwo stałe te same co w rakiecie Thor Delta D. Nowością był nowy człon drugi oraz przestrzeń ładunkowa, wzięta z członu Agena. (pl)
  • O Delta E e a sua variante Delta E1 foram uns foguetes espaciais estadunidense que prestou serviço entre 1965 e 1971. (pt)
  • Thor Delta E или Delta E — американская ракета-носитель семейства Дельта, использовавшаяся с 1965 до 1971 года. (ru)
dbo:finalFlight
  • 1971-04-01 (xsd:date)
dbo:launchSite
dbo:maidenFlight
  • 1965-11-06 (xsd:date)
dbo:rocketFunction
dbo:status
  • Retired
dbo:successfulLaunches
  • 23 (xsd:nonNegativeInteger)
dbo:thumbnail
dbo:totalLaunches
  • 23 (xsd:nonNegativeInteger)
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 17978307 (xsd:integer)
dbo:wikiPageLength
  • 2781 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1084018908 (xsd:integer)
dbo:wikiPageWikiLink
dbp:caption
  • Launch of a Delta E with Pioneer 6 (en)
dbp:countryOrigin
  • United States (en)
dbp:first
  • 1965-11-06 (xsd:date)
dbp:function
dbp:last
  • 1971-04-01 (xsd:date)
dbp:launches
  • 23 (xsd:integer)
dbp:sites
dbp:status
  • Retired (en)
dbp:success
  • 23 (xsd:integer)
dbp:wikiPageUsesTemplate
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • Thor Delta E – amerykańska rakieta nośna z rodziny Thor Delta. Istniały jej dwa warianty: E (6 startów) i E1 (17 startów). Obydwie wersje wykorzystywały centralny człon i dopalacze na paliwo stałe te same co w rakiecie Thor Delta D. Nowością był nowy człon drugi oraz przestrzeń ładunkowa, wzięta z członu Agena. (pl)
  • O Delta E e a sua variante Delta E1 foram uns foguetes espaciais estadunidense que prestou serviço entre 1965 e 1971. (pt)
  • Thor Delta E или Delta E — американская ракета-носитель семейства Дельта, использовавшаяся с 1965 до 1971 года. (ru)
  • 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. (en)
rdfs:label
  • Delta E (en)
  • Thor Delta E (pl)
  • Delta E (pt)
  • Дельта-E (ru)
owl:sameAs
prov:wasDerivedFrom
foaf:depiction
foaf:isPrimaryTopicOf
is dbo:launchVehicle of
is dbo:maidenFlightRocket of
is dbo:wikiPageWikiLink of
is dbp:launchRocket of
is dbp:launcher of
is dbp:maidens of
is foaf:primaryTopic of
Powered by OpenLink Virtuoso    This material is Open Knowledge     W3C Semantic Web Technology     This material is Open Knowledge    Valid XHTML + RDFa
This content was extracted from Wikipedia and is licensed under the Creative Commons Attribution-ShareAlike 3.0 Unported License