Titan IVB/Centaur

E202552

Titan IVB/Centaur was a heavy-lift U.S. expendable launch vehicle configuration that combined the Titan IVB rocket with a Centaur upper stage to send large payloads, such as the Cassini–Huygens spacecraft, on deep-space missions.

All labels observed (4)

Label Occurrences
Titan IV Centaur 1
Titan IV-Centaur 1
Titan IV/Centaur 1

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf expendable launch vehicle configuration ⓘ
heavy-lift launch vehicle ⓘ
capability interplanetary injection ⓘ
configuration two solid rocket boosters plus liquid-fueled core plus Centaur upper stage ⓘ
countryOfOrigin United States ⓘ
customerForCassini–Huygens NASA ⓘ
designFeature high-energy cryogenic upper stage ⓘ
developedFrom Titan IV/Centaur ⓘ
linked to: Titan IVB/Centaur
era 1990s ⓘ
family Titan rocket family ⓘ
launchCapability heavy payloads to geostationary transfer orbit ⓘ
planetary trajectories ⓘ
launchOfCassini–Huygens 15 October 1997 ⓘ
launchSite Cape Canaveral Air Station Space Launch Complex 40 ⓘ
Cape Canaveral Air Station Space Launch Complex 41 ⓘ
Vandenberg Air Force Base Space Launch Complex 4E ⓘ
launchSiteOfCassini–Huygens Cape Canaveral Air Station Space Launch Complex 40 ⓘ
launchVehicleFamily Titan IV ⓘ
launchVehicleRole interplanetary science missions ⓘ
national security payloads ⓘ
lowerStage Titan IVB ⓘ
linked to: Titan IV
manufacturer Lockheed Martin ⓘ
Martin Marietta ⓘ
missionTypeForCassini–Huygens Saturn orbiter and Titan lander ⓘ
notablePayload Cassini–Huygens ⓘ
operator United States Air Force ⓘ
primaryUse deep-space missions ⓘ
high-energy Earth orbit missions ⓘ
program Titan IV program ⓘ
propellantTypeCoreStage Aerozine 50 ⓘ
dinitrogen tetroxide ⓘ
propellantTypeFirstStage solid rocket propellant ⓘ
propellantTypeUpperStage liquid hydrogen ⓘ
liquid oxygen ⓘ
retirementReason replacement by Evolved Expendable Launch Vehicle program ⓘ
stageCount 3 ⓘ
status retired ⓘ
successor Atlas V ⓘ
Delta IV Heavy ⓘ
upperStage Centaur ⓘ
upperStageDeveloper Convair ⓘ
General Dynamics ⓘ
upperStageEngineType RL10 ⓘ
upperStageLaterManufacturer Lockheed Martin ⓘ
upperStageVariant Centaur T ⓘ
usedBy National Aeronautics and Space Administration ⓘ
linked to: NASA

United States Air Force ⓘ

How these facts were elicited

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

Cassini–Huygens → launchVehicle → Titan IVB/Centaur ⓘ
Titan IIIE-Centaur → successor → Titan IV-Centaur ⓘ
linked to: Titan IVB/Centaur
Titan IVB/Centaur → developedFrom → Titan IV/Centaur ⓘ
linked to: Titan IVB/Centaur
Centaur T → usedOnLaunchVehicleVariant → Titan IV Centaur ⓘ
linked to: Titan IVB/Centaur