📊 Analysis
Statistics & insights on rockets and organizations — technology, history, numbers.
Titan II GLV
RetiredNational Aeronautics and Space Administration
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.
Key figures
Total launches
12
Successes
12
Failures
0
Success rate
100.0 %
Success streak
12
Maiden flight
Apr 8, 1964
Reusable
No
Shortest launch interval ⓘ
10d 18h
Planned launches
0
Titan, Titan II family total
25 launches · 24 successes · 1 failures (2 variants)
🧐 Data check
Automatic plausibility checks — anomalies are surfaced transparently here:
- ℹ️The figures above apply only to the “Titan II GLV” variant. The Launch Library counts each variant separately — the Titan, Titan II family totals 25 launches across 2 variants.
Technology
Length
33.2 m
Diameter
3.05 m
Launch mass
154 t
Liftoff thrust
1,913 kN
Stages
2
LEO (low Earth orbit)
3,850 kg
Launches per year
of which in our database: 12
Successes Failures Other/planned
History & events
Sources
- Launch Library 2 (The Space Devs)
- Wikipedia