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.

All labels observed (2)

Label Occurrences
Titan 23G canonical 2
Titan II(23)G 1

How this entity was disambiguated

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 ⓘ
derivedFrom Titan II ICBM ⓘ
era Cold War ⓘ
post–Cold War ⓘ
family Titan rocket family ⓘ
firstLaunchDate 1988-03-14 ⓘ
firstStageOxidizer nitrogen tetroxide ⓘ
firstStagePropellant Aerozine 50 ⓘ
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 ⓘ
Space Launch Complex 4W ⓘ
launchesSuccessful 13 ⓘ
launchesTotal 13 ⓘ
launchPeriodEnd 2003 ⓘ
launchPeriodStart 1988 ⓘ
launchSite Vandenberg Air Force Base ⓘ
launchVehicleType converted ICBM ⓘ
manufacturer Martin Marietta ⓘ
numberOfStages 2 ⓘ
operator United States Air Force ⓘ
payloadToLEO approximately 1900 kilograms ⓘ
propellantType hypergolic ⓘ
secondStageOxidizer nitrogen tetroxide ⓘ
secondStagePropellant Aerozine 50 ⓘ
status retired ⓘ
successor Atlas II ⓘ
Delta II ⓘ
successRate 100 percent ⓘ
usedBy United States Air Force ⓘ
United States Department of Defense ⓘ
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 ⓘ

How these facts were elicited

Referenced by (3)

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

Clementine mission → launchVehicle → Titan II(23)G ⓘ
linked to: Titan 23G