USAF Titan II GLV Gemini II
Titan II GLV
Status
Success
Date
19 JAN 1965
14:04
Mission Overview
Uncrewed test flight of the Gemini capsule.
Rocket
Titan II GLV
Mission Type
Test Flight
Orbit
Suborbital
Stages
2
Livestream
Not availableRocket Details
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.
Height
33.2 m
Diameter
3.05 m
Launch Mass
154 T
Thrust
1,913 kN