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 (3)

Label Occurrences
Titan IV-Centaur 1
Titan IV/Centaur 1
Titan IVB/Centaur canonical 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 of America
surface form: United States
customerForCassini–Huygens NASA
designFeature high-energy cryogenic upper stage
developedFrom Titan IVB/Centaur self-linksurface differs
surface form: Titan IV/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 Force Station Space Launch Complex 40
surface form: Cape Canaveral Air Station Space Launch Complex 40

Cape Canaveral LC-41
surface form: Cape Canaveral Air Station Space Launch Complex 41

Space Launch Complex 4
surface form: Vandenberg Air Force Base Space Launch Complex 4E
launchSiteOfCassini–Huygens Cape Canaveral Air Force Station Space Launch Complex 40
surface form: Cape Canaveral Air Station Space Launch Complex 40
launchVehicleFamily Titan IV
launchVehicleRole interplanetary science missions
national security payloads
lowerStage Titan IV
surface form: Titan IVB
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 launch vehicle
surface form: 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 NASA
surface form: National Aeronautics and Space Administration

United States Air Force

How these facts were elicited

Referenced by (3)

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 IVB/Centaur
this entity surface form: Titan IV-Centaur
Titan IVB/Centaur developedFrom Titan IVB/Centaur self-linksurface differs
this entity surface form: Titan IV/Centaur