Gemini-Titan II
A Titan II on the launch pad (NASA Photo)
The first manned Gemini-Titan II, carry the Gemini 3 mission, standing atop the pad with the gantry lowering. (NASA)

    The Gemini program needed a large booster to launch the larger two-place Gemini spacecraft. The Atlas D, used for the orbital Mercury launches, would not be sufficient. NASA decided to use the Titan II InterContinental Ballistic Missile (ICBM). The two-staged Titan II burned hypergolic (igniting on contact) could lift a payload of 3,100 kg to a 185 km LEO (Low Earth Orbit). This would work well for Gemini.
    NASA made a contract with McDonnell Douglas to build several upgraded Titan IIs with special backup systems to man-rate the boosters, as requested. Twelve flights in total were flown on the Gemini program, ten of which were manned.

Gemini-Titan II specifications
Country: USA
Organization: NASA
Stages: 2
Length: 30.1 meters
Diameter: 3.1 meters
Mass: 150,530 kilograms
Cost: $16,240,000