Titan II SLV Vehicle Overview

A complete overview of the Titan II SLV launch vehicle, including launch stats, vehicle info and launch locations.

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Titan II SLV rocket

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

Vandenberg SFB launch site

U.S. Space Force facility in California for spacecraft launches and missile testing.

📍 CA, United States
🚀 797 Launches

Upcoming Launches