The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar and Manned Orbiting Laboratory, though both programs were cancelled before any astronauts flew. The majority of the launcher's payloads were DoD satellites, namely for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

Property Value
dbo:MeanOfTransportation/diameter
  • 3.048
dbo:MeanOfTransportation/height
  • 41757.6
dbo:MeanOfTransportation/mass
  • 626199.336
dbo:Rocket/lowerEarthOrbitPayload
  • 13109.04
dbo:Rocket/mass
  • 626199.336
dbo:abstract
  • The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar and Manned Orbiting Laboratory, though both programs were cancelled before any astronauts flew. The majority of the launcher's payloads were DoD satellites, namely for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB. (en)
  • O Titan IIIC, foi um veículo de lançamento descartável de origem Norte americana. Fabricado pela Martin Marietta, foi desenvolvido em 1965, e suportava cargas úteis de grande porte. O Titan IIIC, consistia de um núcleo movido a combustível líquido e dois motores auxiliares laterais, movidos a combustível sólido. O núcleo desse modelo, consistia de três estágios: * O primeiro, usava um motor LR-87 (com duas câmaras de combustão), e a combinação de Aerozine 50 e NTO como propelentes. * O segundo, usava um motor LR-91, montado numa estrutura com o mesmo diâmetro do primeiro, e usando a mesma mistura de propelentes. * O terceiro, conhecido como Titan Transtage tinha a capacidade de ter o seu funcionamento interrompido e reiniciado, usando a mesma mistura de propelentes. (pt)
  • Titan 3C – wykorzystywana przez USAF rakieta nośna serii Titan, największa amerykańska wojskowa rakieta nośna w latach 1965-1982 (do czasu wyprodukowania pierwszej rakiety Titan IV). Planowana była jako rakieta dla samolotu Boeing X-20 Dyna-Soar i pojazdów MOL. Jej konstrukcja oparta jest na rakiecie Titan 3A, zaś dołączone są również dopalacze na paliwo stałe, za pomocą których rakieta wynoszona była w przestworza, po ich odłączeniu załączany był silnik 1. stopnia. Rakieta ta stała się bazą dla rakiet Titan 3D (odmiana bez stopnia Transtage) oraz Titan 3E (wersja 3C z stopniem Centaur zamiast Transtage). (pl)
  • «Титан-3C» — американская ракета-носитель тяжелого класса, семейства Титан. (ru)
dbo:countryOrigin
dbo:diameter
  • 3.048000 (xsd:double)
dbo:failedLaunches
  • 5 (xsd:integer)
dbo:finalFlight
  • 1982-03-06 (xsd:date)
dbo:height
  • 41.757600 (xsd:double)
dbo:launchSite
dbo:lowerEarthOrbitPayload
  • 13109040.000000 (xsd:double)
dbo:maidenFlight
  • 1965-06-18 (xsd:date)
dbo:manufacturer
dbo:mass
  • 626199336.000000 (xsd:double)
dbo:rocketStages
  • 2 (xsd:integer)
dbo:status
  • Retired
dbo:successfulLaunches
  • 31 (xsd:integer)
dbo:thumbnail
dbo:totalLaunches
  • 36 (xsd:integer)
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 843195 (xsd:integer)
dbo:wikiPageRevisionID
  • 740377453 (xsd:integer)
dbp:altDiameter
  • 3.05m
dbp:altHeight
  • 42 m
dbp:altLeo
  • 13100.0
dbp:altMass
  • 626190.0
dbp:altPayload
  • 3000.0
  • 1200.0
dbp:caption
  • Launch of a Titan IIIC
dbp:family
dbp:function
  • Medium/Heavy launch vehicle
dbp:payload
  • 6600.0
  • 2650.0
dbp:payload2Location
dbp:payloadLocation
dct:subject
http://purl.org/linguistics/gold/hypernym
rdf:type
rdfs:comment
  • The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar and Manned Orbiting Laboratory, though both programs were cancelled before any astronauts flew. The majority of the launcher's payloads were DoD satellites, namely for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB. (en)
  • «Титан-3C» — американская ракета-носитель тяжелого класса, семейства Титан. (ru)
  • Titan 3C – wykorzystywana przez USAF rakieta nośna serii Titan, największa amerykańska wojskowa rakieta nośna w latach 1965-1982 (do czasu wyprodukowania pierwszej rakiety Titan IV). Planowana była jako rakieta dla samolotu Boeing X-20 Dyna-Soar i pojazdów MOL. Jej konstrukcja oparta jest na rakiecie Titan 3A, zaś dołączone są również dopalacze na paliwo stałe, za pomocą których rakieta wynoszona była w przestworza, po ich odłączeniu załączany był silnik 1. stopnia. (pl)
  • O Titan IIIC, foi um veículo de lançamento descartável de origem Norte americana. Fabricado pela Martin Marietta, foi desenvolvido em 1965, e suportava cargas úteis de grande porte. O Titan IIIC, consistia de um núcleo movido a combustível líquido e dois motores auxiliares laterais, movidos a combustível sólido. O núcleo desse modelo, consistia de três estágios: (pt)
rdfs:label
  • Titan IIIC (en)
  • Titan 3C (pl)
  • Titan IIIC (pt)
  • Titan IIIC (ru)
owl:sameAs
prov:wasDerivedFrom
foaf:depiction
foaf:isPrimaryTopicOf
foaf:name
  • Titan IIIC (en)
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