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Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA.The Titan II used the LR-87-5 engine, a modified version of the LR-87, that used a hypergolic propellant combination of nitrogen tetroxide (NTO) for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and unsymmetrical dimethylhydrazine (UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I.
The last Titan II missile, located at Silo 373-8 near Judsonia, Arkansas, was deactivated on 5 May 1987. With their warheads removed, the deactivated missiles were initially placed in storage at Davis–Monthan Air Force Base , Arizona, and the former Norton Air Force Base , California, but were later broken up for salvage by 2009.
LGM-25C Titan II, Silo Launch Test Facility for Titan II. Launched a Titan I on 3 May 1961. The facility was first built as a design and construction test for a mission-firing silo. Later, it became the Titan II Operations and Maintenance Missile Trainer (QMT). [7] [11] LC-A
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Launch of a Titan 34D with two UA1206 boosters. UA120 was a family of American solid rocket boosters, manufactured by the Chemical Systems Division of United Aircraft (later United Technologies Corporation). [1] They were used as strap-on boosters for the Titan rocket family. [2] Several variants existed, with a varying number of segments.
The Martin Marietta SM-68A/HGM-25A Titan I was the United States' first multistage intercontinental ballistic missile (ICBM), in use from 1959 until 1962. Though the SM-68A was operational for only three years, it spawned numerous follow-on models that were a part of the U.S. arsenal and space launch capability.
The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles.While the original version - the LR91-3 - ran on RP-1/LOX (as did the companion LR87-3) on the Titan I, the models that propelled the Titan II and later were switched to Aerozine 50/N 2 O 4.
The leak occurred due to puncture of the first-stage Titan fuel tank by a dropped tool. The initial explosion removed the 740-ton silo door and ejected the second stage and warhead out of the silo. The Titan's second stage exploded, and the W53 warhead landed 30 meters from the silo portal without detonating or leaking fissile material .