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Titan II missile. Part of the Titan rocket family, the Titan II ICBM was the successor to the Titan I, with double the payload. Unlike the Titan I, it used hydrazine -based hypergolic propellant which was storable and reliably ignited. This reduced time to launch and permitted it to be launched from its silo.
TITAN II FACT SHEET. By Cliff Lethbridge. Titan II On Launch Pad, Photo Courtesy U.S. Air Force. Classification: Inter-Continental Ballistic Missile. Length: 102 feet. Diameter: 10 feet. Range: 9,325 miles. Date of First Cape Canaveral Launch: March 16, 1962. Date of Final Cape Canaveral Launch: April 9, 1964.
The Titan I and Titan II were part of the US Air Force's intercontinental ballistic missile (ICBM) fleet until 1987. The space launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed flights of the mid-1960s.
Feb 2, 2024 · The Titan II Missile program was a Cold War weapons system featuring fifty-four launch complexes in three states. Eighteen launch complex sites were in Arkansas, from which intercontinental ballistic missiles carrying nine-megaton nuclear warheads could be launched to strike targets as far as 5,500 miles away.
Apr 23, 2024 · The LGM-25C Titan II was the last liquid-fueled intercontinental ballistic missile (ICBM) built by the United States. It was in service between 1963-1987 and could range 15,000 km.
Carrying the largest nuclear warhead ever deployed on an ICBM by the United States, and with a range of 5,500 miles, the Titan II was the ultimate liquid-propellant ICBM. Fifty-four Titan II ICBMs were deployed in groups of eighteen around three Air Force Bases, with the first units coming on alert in early 1963.
Titan II - Originally designated the SM-68B, WS-107B, later designated the LGM-25C. Development approved in October 1959, a large, two stage hypergolic fueled missile. Hypergolic fuels are stored in the missile and ignite on contact, providing immediate response.
