Length: 33.2 m
Diameter: 3.05 m
Launch Mass: 154 T
Low Earth Orbit Capacity: 3850 kg
The Titan II GLV was manufactured by National Aeronautics and Space Administration with the first launch on 1964-04-08. Titan II GLV has 12 successful launches and 0 failed launches with a total of 12 launches. The Titan II GLV (Gemini Launch Vehicle) or Gemini-Titan II was an American expendable launch system derived from the Titan II missile, which was used to launch twelve Gemini missions for NASA between 1964 and 1966. Two unmanned launches followed by ten manned ones were conducted from Launch Complex 19 at the Cape Canaveral Air Force Station, starting with Gemini 1 on April 8, 1964.