Titan II GLV Vehicle Overview
A complete overview of the Titan II GLV launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Titan II GLV
Family
Titan
Manufacturer
First Launch
8 Apr 1964
Successful Launches
12
Failed Launches
0
Rocket Info
Status
Inactive
Stages
2
Length
33.2 m
Diameter
3.05 m
Launch Mass
154 tons
Thrust
1,913 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
3,850 kg
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.
Launch Sites used by Titan II GLV
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.