Titan II SLV
In-activeLockheed Martin (LMT)
Sept. 5, 1988
Description
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.
Specifications
-
Minimum Stage
2 -
Max Stage
3 -
Length
31.4 m -
Diameter
3.05 m -
Fairing Diameter
3.05 m -
Launch Mass
117.0 T -
Thrust
1900.0 kN
Family
-
Name
Titan II SLV -
Family
― -
Variant
23G -
Alias
― -
Full Name
Titan II SLV
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
3600.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Lockheed Martin
Commercial
None
LMT 1953Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.
Flight Record
No spaceflights found for .
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