Titan 23G

E924791

Titan 23G was an American expendable launch vehicle derived from decommissioned Titan II ICBMs and used primarily in the 1980s and 1990s to place military and scientific payloads into orbit.

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All labels observed (2)

Label Occurrences
Titan 23G canonical 1
Titan II(23)G 1

Statements (47)

Predicate Object
instanceOf expendable launch vehicle
orbital launch vehicle
basedOn Titan II GLV design
configuration two-stage liquid-fueled rocket
countryOfOrigin United States of America
surface form: United States
derivedFrom Titan II ICBM NERFINISHED
era Cold War
post–Cold War
family Titan rocket family NERFINISHED
firstLaunchDate 1988-03-14
firstStageOxidizer nitrogen tetroxide
firstStagePropellant Aerozine 50 NERFINISHED
fuelType storable liquid propellants
lastLaunchDate 2003-10-17
launchAzimuthRange primarily polar and sun-synchronous trajectories
launchCapability low Earth orbit
polar orbit
sun-synchronous orbit
launchComplex Space Launch Complex 4E NERFINISHED
Space Launch Complex 4W NERFINISHED
launchesSuccessful 13
launchesTotal 13
launchPeriodEnd 2003
launchPeriodStart 1988
launchSite Vandenberg Air Force Base NERFINISHED
launchVehicleType converted ICBM
manufacturer Martin Marietta NERFINISHED
numberOfStages 2
operator United States Air Force
payloadToLEO approximately 1900 kilograms
propellantType hypergolic
secondStageOxidizer nitrogen tetroxide
secondStagePropellant Aerozine 50
status retired
successor Atlas II NERFINISHED
Delta II NERFINISHED
successRate 100 percent
usedBy United States Air Force
United States Department of Defense NERFINISHED
usedDecommissionedHardware Titan II ICBM first stages
Titan II ICBM second stages
usedFor Earth observation satellites
launching military payloads
launching research satellites
launching scientific payloads
meteorological satellites
technology demonstration payloads

Referenced by (2)

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

Clementine mission launchVehicle Titan 23G
this entity surface form: Titan II(23)G