USAF Titan II GLV Gemini I
Titan II GLV
Status
Success
Date
8 APR 1964
16:00
Mission Overview
Gemini 1 was the first mission in NASA's Gemini program. An uncrewed test flight of the Gemini spacecraft, its main objectives were to test the structural integrity of the new spacecraft and modified Titan II launch vehicle. It was also the first test of the new tracking and communication systems for the Gemini program and provided training for the ground support crews for the first crewed missions.
Rocket
Titan II GLV
Mission Type
Test Flight
Orbit
Low Earth Orbit
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