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.
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Identity
- Aliases
- Gemini Launch VehicleGemini-Titan IITitan II GLV
- Family Name
- Titan II GLV
- Full Name
- 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.
- Dimensions
- Diameter M
- 3
- Height M
- 27.4
- First Flight Year
- 1,964
- Last Flight Year
- 1,966
- Operator
- Parent Vehicle Family
- Propulsion Configurations
- Entries
- Nested value
- Nested value
- Rocket Specs
- Liftoff Mass Kg
- 150,000
- Reusability
- expendable
Links
- Official Url
- https://sma.nasa.gov/LaunchVehicle/titanglv.html
- Wikipedia Url
- https://en.wikipedia.org/wiki/Titan_II_GLV
Assets & Meta
- Creation Time
- July 13, 2026 at 08:25:54 UTC
- Updated Time
- July 29, 2026 at 15:42:44 UTC
- Image
- Download
Other
- Search Name
- Titan II Gemini Launch Vehicle Gemini Launch Vehicle Gemini-Titan II Titan II GLV