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Commercial Titan III

Titan familyLockheed MartinRetired

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.

Commercial Titan III vehicle

Specifications

Thrust
12,450 kN
Height
47.3 m
Diameter
3.05 m
Launch mass
680 t
Stages
3
Launch cost
$136.6M
LEO capacity
14,742 kg
GTO capacity
4,990 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

4flightswith a definitive outcome
100%success rate4 of 4
4success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

4 of 4