Titan II GLV
Titan family
· built by National Aeronautics and Space Administration
· maiden flight 1964-04-08
Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-17
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
33.2 mLength
3.05 mDiameter
154 tLaunch mass
2Stages
1913 kNLiftoff thrust
Payload Capacity
3850 kgTo LEO
Lifetime Launch Record
As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.
12Total launches
12Successful
0Failed
0Upcoming
Launches Tracked on This Site
12In our archive
100.0%Success rate
Apr 08, 1964 16:00 UTCEarliest tracked
Nov 11, 1966 20:46 UTCMost recent
| Mission | Date | Status |
|---|---|---|
| Titan II GLV | Gemini XII | Nov 11, 1966 20:46 UTC | Success |
| Titan II GLV | Gemini XI | Sep 12, 1966 14:42 UTC | Success |
| Titan II GLV | Gemini X | Jul 18, 1966 22:20 UTC | Success |
| Titan II GLV | Gemini IX-A | Jun 03, 1966 13:39 UTC | Success |
| Titan II GLV | Gemini VIII | Mar 16, 1966 16:41 UTC | Success |
| Titan II GLV | Gemini VI-A | Dec 15, 1965 13:37 UTC | Success |
| Titan II GLV | Gemini VII | Dec 04, 1965 19:30 UTC | Success |
| Titan II GLV | Gemini V | Aug 21, 1965 14:00 UTC | Success |
| Titan II GLV | Gemini IV | Jun 03, 1965 15:16 UTC | Success |
| Titan II GLV | Gemini III | Mar 23, 1965 14:24 UTC | Success |
| Titan II GLV | Gemini II | Jan 19, 1965 14:04 UTC | Success |
| Titan II GLV | Gemini I | Apr 08, 1964 16:00 UTC | Success |