Titan II GLV
Titan family · National Aeronautics and Space Administration · Retired
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.
Specifications
- Thrust
- 1,913 kN
- Height
- 33.2 m
- Diameter
- 3.05 m
- Launch mass
- 154 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 3,850 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
12
Launches with a definitive outcome
Success rate
100%
12 of 12
Current success streak
12
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Titan II GLV | Gemini XII — Success
- Titan II GLV | Gemini XI — Success
- Titan II GLV | Gemini X — Success
- Titan II GLV | Gemini IX-A — Success
- Titan II GLV | Gemini VIII — Success