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Titan was a family of United States expendable rockets used between 1959 and 2005. 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
Titan II rocket launch with Clementine spacecraft (25 January 1994) Titan-II 23G-9 B-107 carrying DMSP-5D3 F-16 Final Titan II launch 18 Oct 2003 The first flight of the Titan II was in March 1962 and the missile, now designated LGM-25C, reached initial operating capability in October 1963.
First flight of Titan IV. An engine bell burn-through left only a narrow margin for success. 4 September 05:54 Titan 34D/Transtage: 5D-7 34D-2 CCAFS LC-40: HEO: Success USA-43 USA-44 Final flight of Titan 34D; final use of the Transtage upper stage 6 September 01:49 Titan II(23)G: 23G-2 B-99 B-75 VAFB SLC-4W: LEO: Success USA-45
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.
This page is an incomplete list of orbital rocket engine data and specifications. Current, upcoming, and in-development rocket engines ... Titan IV: Booster: PBAN ...
Spacecraft launched by Titan rockets (25 P) Pages in category "Titan (rocket family)" The following 17 pages are in this category, out of 17 total.
Titan II (SM-68B, LGM-25C): Former hypergolic-fueled ICBM launched from silo, the rocket was used in 1965-1966 for ten crewed Gemini flights and its two-stage core was modified into the heavy-lifting Titan III and Titan IV rockets. All Titan II, III, and IV models have since been retired. Minuteman I (SM-80, LGM-30A/B, HSM-80) Minuteman II (LGM ...
The LR87 was an American liquid-propellant rocket engine used on the first stages of Titan intercontinental ballistic missiles and launch vehicles. [1] Composed of twin motors with separate combustion chambers and turbopump machinery, [2] it is considered a single unit and was never flown as a single combustion chamber engine or designed for this.