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  2. Titan IIIE - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIE

    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 .

  3. Titan IIIC - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIC

    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.

  4. Titan IIIB - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIB

    The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing , in order to allow larger payloads to be launched.

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  6. Commercial Titan III - Wikipedia

    en.wikipedia.org/wiki/Commercial_Titan_III

    The Commercial Titan III, also known as CT-3 or CT-III, was an American expendable launch system, developed by Martin Marietta during the late 1980s and flown four times during the early 1990s. It was derived from the Titan 34D , and was originally proposed as a medium-lift expendable launch system for the US Air Force , who selected the Delta ...

  7. Titan IIIA - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIA

    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.

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