Category:Titan 23G

**Titan 23G**
	American expendable launch vehicle
	Upload media
	Wikipedia
Instance of	rocket model; weapon model;
Subclass of	LGM-25C Titan II;
Country of origin	United States of America;
Based on	LGM-25C Titan II;
Has part(s)	LR-87 (1); LR-91 (2); STAR 37 (optional, 3);
Start point	Vandenberg Space Force Base Space Launch Complex 4 West;
Manufacturer	Martin Marietta;
Service entry	5 September 1988;
Service retirement	18 October 2003;
Source of energy	Aerozine-50 (combustible matter); dinitrogen tetroxide (oxidizing agent);
Mass	154,000 kg (gross weight);
Diameter	3.05 m;
Height	31.4 m (baseline);
Authority file
	Q5918827;
	Reasonator; Scholia; Wikidocumentaries; PetScan; statistics; WikiMap; Locator tool; KML file; Search depicted;

English: Titan 23G - The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American expendable launch system derived from the LGM-25C Titan II intercontinental ballistic missile.