National Aeronautics and Space Administration
Titan II GLV
GLV

Retired
Overview
/01The 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.
Manufacturer
National Aeronautics and Space Administration
Variant
GLV
Alias
N/A
Maiden Flight
April 8, 1964
Technical Specifications
/0233.2 m
Length
3.05 m
Diameter
0 t
Launch Mass
1913 kN
Liftoff Thrust
3850 kg
LEO Capacity
—
GTO Capacity
Launch Record
/0312
Total Launches
12
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes