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Titan · Lockheed Martin

Titan II SLV

retired
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Specifications

Status
retired
Height
31.4 m
Diameter
3.05 m
Mass
117,000 kg
Stages
3
Payload to LEO
3,600 kg
First flight
1988-09-05
Total launches
13
Success / Fail
12 / 1

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.

Payloads it launched · 12

DMSP 5D-3 F16 (USA 172)
LEO
CORIOLIS
LEO
NOAA 17
LEO
NOAA 16
LEO
DMSP 5D-3 F15 (USA 147)
LEO
QUIKSCAT
LEO
NOAA 15
LEO
DMSP 5D-2 F14 (USA 131)
LEO
CLEMENTINE 1 (DSPSE)
Heliocentric
USA 81
LEO
USA 45
Payload
USA 32
LEO