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NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

Titan II

12FLIGHTS
100%SUCCESS
12STREAK
Apr 1964FIRST FLIGHT
NOREUSABLE
HEIGHT33.2 m
DIAMETER3.05 m
LAUNCH MASS154 kg
LIFTOFF THRUST1,913 kN
STAGES2

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.

3,850 kg
TO LEO
8,489 lbs
1,913
KILONEWTONS
430,060
POUNDS-FORCE
~2,565
HORSEPOWER
Height33.2 m (109 ft)
Diameter3.05 m (10 ft)
Launch Mass154 kg (340 lbs)
Stages2