Titan·Lockheed Martin
Titan II GLV
retired
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Specifications
- Status
- retired
- Height
- 33.2 m
- Diameter
- 3.05 m
- Mass
- 154,000 kg
- Stages
- 2
- Thrust
- 1,913 kN
- Payload to LEO
- 3,850 kg
- First flight
- 1964-04-08
- Total launches
- 12
- Success / Fail
- 12 / 0
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.
Payloads it launched
13 loaded