Titan II SLV Vehicle Overview
A complete overview of the Titan II SLV launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Titan II SLV
Family
Titan
Manufacturer
First Launch
5 Sep 1988
Successful Launches
12
Failed Launches
1
Rocket Info
Status
Inactive
Stages
2-3
Length
31.4 m
Diameter
3.05 m
Launch Mass
117 tons
Thrust
1,900 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
3,600 kg
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.
Launch Sites used by Titan II SLV
Vandenberg SFB
U.S. Space Force facility in California for spacecraft launches and missile testing.