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LGM-25C Titan II

Launch vehicle
The Titan II was an intercontinental ballistic missile developed by the Glenn L. Martin Company from the earlier Titan I missile. Wikipedia
Height: 103.00 ft
Engine: Two-stage liquid-fueled rocket engines; first stage: LR-87; second stage: LR91
Guidance system: Inertial IBM ASC-15
In service: 1962 to 1987
Launch platform: Missile silo
Warhead: W-53 9 Mt thermonuclear warhead