Titan II Gemini Launch Vehicle
The Titan II Gemini Launch Vehicle was a human-rated two-stage derivative of the Titan II intercontinental ballistic missile developed for Project Gemini. It used storable hypergolic propellants and launched the two uncrewed Gemini qualification flights and all ten crewed Gemini missions between 1964 and 1966.
Identity
- Aliases
- Gemini Launch VehicleGemini-Titan IITitan II GLV
- Family Name
- Titan II GLV
- Full Name
- Titan II Gemini Launch Vehicle
- Reusability
- expendable
- Slug
- titan-ii-gemini-launch-vehicle
- Status
- retired
- Type
- rocket
Details
- Description
- The Titan II Gemini Launch Vehicle was a human-rated two-stage derivative of the Titan II intercontinental ballistic missile developed for Project Gemini. It used storable hypergolic propellants and launched the two uncrewed Gemini qualification flights and all ten crewed Gemini missions between 1964 and 1966.
- Diameter M
- 3
- Engines
- Count
- 2
- Name
- Aerojet YLR-87-AJ-7
- Count
- 1
- Name
- Aerojet YLR-91-AJ-7
- First Flight Year
- 1,964
- Height M
- 27.4
- Last Flight Year
- 1,966
- Liftoff Mass Kg
- 150,000
- Operator Id
- vh76vnx3yy1vy23j7zc3wk80wx7nhx5f
- Parent Vehicle Family Id
- nd7n2vycv7g3eyeqpvnadxh7b985jb4m
Links
- Official Url
- https://sma.nasa.gov/LaunchVehicle/titanglv.html
- Wikipedia Url
- https://en.wikipedia.org/wiki/Titan_II_GLV
Assets & Meta
- Creation Time
- 7/13/2026, 8:25:54 AM
- Updated Time
- 7/13/2026, 8:25:54 AM