Q5918827: Difference between revisions

From Spacefaring

Q5918827
Bot: Automated import of articles *** existing text overwritten ***
Bot: Automated import of articles *** existing text overwritten ***
 
Line 1: Line 1:
{{Page|Titan 23G|Classes|American expendable launch vehicle|SLV-5, Titan 2(23)G, Titan 2G, Titan II(23)G, Titan II SLV, Titan II Space Launch Vehicle}}
{{Page|Titan 23G|Classes|American expendable launch vehicle|SLV-5; Titan 2(23)G; Titan 2G; Titan II SLV; Titan II Space Launch Vehicle; Titan II(23)G}}

Latest revision as of 12:52, 2 September 2025




The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American medium-lift launch vehicle derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta, into which the Glenn L. Martin Company, which built the original Titan II, had merged. It was used to carry payloads for the United States Air Force (USAF), NASA and National Oceanic and Atmospheric Administration (NOAA). Thirteen were launched from Space Launch Complex 4W (SLC-4W) at the Vandenberg Air Force Base between 1988 and 2003.

1988 — 2003  WikimediaWikidata
SLV-5; Titan 2(23)G; Titan 2G; Titan II SLV; Titan II Space Launch Vehicle; Titan II(23)G
height 31.4 metre, diameter 3.05 metre, mass 154000 kilogram, payload mass 2177 kilogram, payload mass 3175 kilogram, 
LGM-25C Titan IIMartin Marietta, United States
United StatesClementineDong Fang Hong 2EkranLGM-25C Titan II1988


Location: KML, Cluster Map, Maps,

    Titan 23G rocket launchTitan 23G rocket launch
    Dyna-Soar on Titan boosterDyna-Soar on Titan booster
      TypeSubtypeDateDescriptionNotesSource
      commonsimageTitan 23G rocket launch Commons
      commonsimageDyna-Soar on Titan booster Commons