The Titan III family used the same basic LR-87 engines as Titan II (with performance enhancements over the years), however SRB-equipped variants had a heat shield over them as protection from the SRB exhaust and the engines were modified for air-starting.

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.

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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.

A Titan IIIE/Centaur launched from Cape Canaveral boosted the United States-West German HELIOS spacecraft into heliocentric orbit as a solar probe to investigate the properties and processes of solar/terrestrial relationships.

Jan 21, 2022 · The Titan III was a modified Titan II with optional solid rocket boosters.

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With the significant performance improvements which resulted from introducing twin solid rocket boosters, the Titan III-C was able to carry a 29,600-pound payload to low-Earth orbit or a 3,600-pound payload to geostationary transfer orbit.

The Titan 3E was a modified U.S. Air Force Titan missile used to launch deep space probes or satellites into geosynchronous orbits. Most notably, the Titan III-E launched two Viking spacecraft to Mars in 1975. These engines were transferred to …

The Titan III family of space launch vehicles was born out of a need for rockets capable of carrying payloads heavier than those which could be handled by the Atlas-Centaur. Introduced in 1964, the Titan III class of rockets was given a numerical designation of SLV-5.