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{{Page|Commercial Titan III|Classes|American expendable launch vehicle|CT-3 | {{Page|Commercial Titan III|Classes|American expendable launch vehicle|CT-3; CT-III}} | ||
Latest revision as of 12:44, 2 September 2025
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 II instead. Development was continued as a commercial launch system, and the first rocket flew in 1990. Due to higher costs than contemporary rockets such as the Ariane 4, orders were not forthcoming, and the CT-3 was retired in 1992.
1990 — 1992
Wikimedia, Wikidata
CT-3; CT-III
mass 680000 kilogram, height 47.3 metre, payload mass 14515 kilogram, payload mass 1850 kilogram,
Reman, Republic of Haiti, 1990, Titan 34D, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
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