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Titan II SLV

Titan familyLockheed MartinRetired

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. 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, NASA and NOAA. Thirteen were launched from Space Launch Complex 4W at the Vandenberg Air Force Base between 1988 and 2003.

Titan II SLV vehicle

Specifications

Thrust
1,900 kN
Height
31.4 m
Diameter
3.05 m
Launch mass
117 t
Stages
3
LEO capacity
3,600 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

13flightswith a definitive outcome
92.3%success rate12 of 13
9success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 13

All 13 flights