Q5918827: Difference between revisions
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{{Page|Titan 23G|Classes|American expendable launch vehicle}} | {{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}} | ||
Revision as of 13:49, 17 February 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
Wikimedia, Wikidata
SLV-5, Titan 2(23)G, Titan 2G, Titan II(23)G, Titan II SLV, Titan II Space Launch Vehicle
height 31.4 metre, diameter 3.05 metre, mass 154000 kilogram, payload mass 2177 kilogram, payload mass 3175 kilogram,
Martin Marietta, United States,
United States, Clementine, Dong Fang Hong 2, Ekran, LGM-25C Titan II, 1988, 1980s,
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Location: KML, Cluster Map, Maps,
Titan 23G rocket launch
Dyna-Soar on Titan booster| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Titan 23G rocket launch | Commons | ||
| commons | image | Dyna-Soar on Titan booster | Commons | ||
