Titan II GLV
Titan familyNational Aeronautics and Space AdministrationRetired
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
- LEO capacity
- 3,850 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
12flightswith a definitive outcome
100%success rate12 of 12
12success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.