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The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar , though the spaceplane was cancelled before it could fly.
The Titan IIIE or Titan 3E, also known as the Titan III-Centaur, was an American expendable launch system. Launched seven times between 1974 and 1977, [ 4 ] it enabled several high-profile NASA missions, including the Voyager and Viking planetary probes and the joint West Germany-U.S. Helios spacecraft .
Titan 3C launch 22 Dec 1965. OV2-3, along with LES-3, LES-4, and OSCAR 4, was launched on the third Titan IIIC test flight [6] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41 [1] just one second behind schedule. From an initial parking orbit of 194 kilometres (121 mi), the Titan's Transtage boosted into a transfer orbit pending a ...
The Titan II and Titan III boosters could launch Dyna-Soar into Earth orbit, as could the Saturn C-1 (later renamed the Saturn I), and all were proposed with various upper-stage and booster combinations. In December 1961, the Titan IIIC was chosen, [27]: 19 ) but the vacillations over the launch system delayed the project and complicated planning.
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 IIIC: 3C-8 CCAFS LC-41: GTO (intended) HEO (achieved) Partial failure LES-4 LES-3 OV2-3 OSCAR 4: Third burn of the Transtage failed, and payloads failed to achieve GTO. OV2-3 failed to separate from the Transtage. 22 December 14:10 Titan II: B-73 VAFB LC-395-C: Suborbital: Success "Sea Rover" [3]
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The Titan IIIA or Titan 3A was an American expendable launch system, launched four times in 1964 and 1965, [1] to test the Transtage upper stage which was intended for use on the larger Titan IIIC. The Transtage was mounted atop two core stages derived from the Titan II. The Titan IIIA was also used as the core of the Titan IIIC.