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. Both Delta D launches were conducted from Cape Canaveral Air Force Station Launch Complex 17A. The first, on 19 August 1964, carried the Syncom 3 satellite. The last, on 6 April 1965, carried the first commercial communications satellite, Intelsat I.

Property Value
dbo:abstract
  • O Delta D foi um foguete espacial leve dos estadunidense em serviço entre 1964 e 1965. (pt)
  • Thor Delta D – amerykańska rakieta nośna serii Delta. Jest bezpośrednią następczynią Delty C, gdyż ma te same stopnie górne, modyfikacją jest dodanie 3 dopalaczy na paliwo stałe serii Castor 1 pochodzących z rakiet Scout, oraz członu centralnego Thor DSV-2. Obydwie nowe konstrukcje latały na rakietach Thor Agena D. Rakieta ta wyniosła 2 satelity komunikacyjne: Syncom 3 19 sierpnia 1964 i Intelsat 1 5 kwietnia 1965. (pl)
  • «Дельта-D» — американская ракета-носитель лёгкого класса, семейства Дельта. (ru)
  • 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. The main difference between the Delta C and Delta D was the presence of three Castor-1 solid rocket boosters, clustered around the first stage. Both Delta D launches were conducted from Cape Canaveral Air Force Station Launch Complex 17A. The first, on 19 August 1964, carried the Syncom 3 satellite. The last, on 6 April 1965, carried the first commercial communications satellite, Intelsat I. (en)
dbo:countryOrigin
dbo:finalFlight
  • 1965-04-06 (xsd:date)
dbo:launchSite
dbo:maidenFlight
  • 1964-08-19 (xsd:date)
dbo:rocketFunction
dbo:status
  • Retired
dbo:successfulLaunches
  • 2 (xsd:integer)
dbo:thumbnail
dbo:totalLaunches
  • 2 (xsd:integer)
dbo:wikiPageID
  • 21471649 (xsd:integer)
dbo:wikiPageRevisionID
  • 542869410 (xsd:integer)
dbp:caption
  • Launch of a Delta D with Intelsat I
dct:subject
http://purl.org/linguistics/gold/hypernym
rdf:type
rdfs:comment
  • O Delta D foi um foguete espacial leve dos estadunidense em serviço entre 1964 e 1965. (pt)
  • Thor Delta D – amerykańska rakieta nośna serii Delta. Jest bezpośrednią następczynią Delty C, gdyż ma te same stopnie górne, modyfikacją jest dodanie 3 dopalaczy na paliwo stałe serii Castor 1 pochodzących z rakiet Scout, oraz członu centralnego Thor DSV-2. Obydwie nowe konstrukcje latały na rakietach Thor Agena D. Rakieta ta wyniosła 2 satelity komunikacyjne: Syncom 3 19 sierpnia 1964 i Intelsat 1 5 kwietnia 1965. (pl)
  • «Дельта-D» — американская ракета-носитель лёгкого класса, семейства Дельта. (ru)
  • 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. Both Delta D launches were conducted from Cape Canaveral Air Force Station Launch Complex 17A. The first, on 19 August 1964, carried the Syncom 3 satellite. The last, on 6 April 1965, carried the first commercial communications satellite, Intelsat I. (en)
rdfs:label
  • Thor Delta D (pl)
  • Delta D (pt)
  • Дельта-D (ru)
  • Delta D (en)
owl:sameAs
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