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Space · launch vehicle

Titan II GLV

NASA RETIRED
At a glance
Launches
12
Success rate
100%
12 ok · 0 failed
Payload to LEO
3,850 kg
Payload to GTO
—
Status
Retired
First flight
08 Apr 1964
Reusable
No
Height
33.2 m
Diameter
3.05 m
Launch mass
154 t
Liftoff thrust
1,913 kN
Stages
2
Launch cost
—
Booster landings
—
About

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.